- Earth-watching satellite
- TOPEX/POSEIDON
- NORAD 22076
- 1992-052A
- Low Earth orbit
Current orbit
View on live mapOrbit began over the Southern Ocean
Orbit ends over the Southern Ocean
Sunlit since
Enters the Earth’s shadow
In view from you
Nobody watches Topex-Poseidon go over, but a receiver still asks whether it is above the horizon. Say where you are and this card answers.
Your position is rounded to about a kilometre and sent only to the Orbinauts API, to find the pass.
No brightness has been published for Topex-Poseidon, so it is not a naked-eye satellite and no city page carries pass times for it. Nothing here estimates one.
Seeing it
There is nothing to go outside for: it is too faint for the naked eye. What it is up there for reaches the ground as pictures and measurements, not as a light in the sky.
Timeline
- Launch
Launched, on the day GCAT records. Source
Summary
Over Mexico LIVE
Where is Topex-Poseidon?
At 5:36:24 PM UTC Topex-Poseidon was over Mexico (26.5° N, 107.5° W), 1,343 km up, moving at 7.19 km/s and in sunlight.
What is Topex-Poseidon?
A satellite that watches the Earth in low Earth orbit, in space since Aug 10, 1992.
Can I see Topex-Poseidon?
No, not with the naked eye: no brightness has been published for Topex-Poseidon, and nothing here estimates one; what people use is its pictures and measurements of the Earth.
General
- Operator
- Jet Propulsion Lab
- State
- United States of America
- Built by
- Fairchild Space and Electronics
- What it is
- Earth-watching satellite
- Launched
- Mass
- about 2.4 t
- Operating
- Orbit class
- Low Earth orbit
From GCAT, Jonathan McDowell’s general catalogue, licensed CC BY 4.0: the operator, the state, the manufacturer, what it is for, the launch day, the mass, and whether it is operating. The orbit class is read from its current elements.
Latest orbital data
- Position received
- 5:36 PM UTC
- Station time (UTC)
- 5:36 PM UTC
- Latitude / longitude
- 26.5° N, 107.5° W
- Altitude
- 1,343 km
- Speed
- 7.19 km/s (25,877 km/h)
- Course
- north-east
- Light
- In sunlight until 6:07 PM UTC
- Inclination
- 66°
- Orbital period
- 112.4 minutes
- Orbits per day
- 12.81
- This orbit
- 1,330 to 1,342 km
- In shadow
- 29 minutes of each orbit
- In view from
- Within 2,840 km of the point below it
- Elements epoch
- Nov 8, 2026, 3:18 AM, 14 hours old
- Source
- Position from Space-Track orbital elements of Nov 8, 2026, 3:18 AM, 14 hours old.
No operator publishes an ephemeris for Topex-Poseidon, so every position here comes from its orbital elements.
In orbit
- Close approaches
- No close approach to Topex-Poseidon has been reported publicly in the past thirty days.
From Space-Track’s public conjunction messages; the latest report was issued Nov 8, 2026, 1:11 PM, 3 hours old. Only approaches serious enough to be reported publicly are listed: within three days and, for two bodies near the Earth, closer than a kilometre with a chance of a collision above 1 in 10,000, the level at which NASA moves the ISS.
Launched with
Topex-Poseidon shares its launch, 1992-052, with 13 other bodies the catalogue lists in orbit.
| Body | What it is |
|---|---|
| OSCAR 23 (KITSAT 1) | Communications satellite |
| S80/T | Communications satellite |
| ARIANE 42P R/B | Rocket body |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB | Debris |
| ARIANE 42P DEB * | Debris |
Read from the international designators of the US catalogue: the year and the launch number every piece of one launch shares. A body that has come down is no longer listed.
Beside the others
| Satellite | Typical altitude | Orbital period | Mass | In space since |
|---|---|---|---|---|
| Topex-Poseidon | 1,330 to 1,342 km | 112 minutes | about 2.4 t | 1992 |
| Sentinel-6MF | 1,332 to 1,344 km | 112 minutes | about 1.2 t | 2020 |
| Sentinel-6B | 1,332 to 1,344 km | 112 minutes | about 1.2 t | 2025 |
| Sentinel-5P | 826 to 828 km | 101 minutes | 820 kg | 2017 |
| Suomi NPP | 825 to 829 km | 101 minutes | about 2.1 t | 2011 |
| MetOp-SG A1 | 820 to 821 km | 101 minutes | about 4 t | 2025 |
Data and API
The current elements from Space-Track as an OMM object, epoch Nov 8, 2026, 3:18 AM, 14 hours old.
{
"OBJECT_NAME": "TOPEX/POSEIDON",
"OBJECT_ID": "1992-052A",
"EPOCH": "2026-11-08T03:18:46.330272",
"MEAN_MOTION": 12.81097524,
"ECCENTRICITY": 0.00078229,
"INCLINATION": 66.0399,
"RA_OF_ASC_NODE": 193.0823,
"ARG_OF_PERICENTER": 267.1978,
"MEAN_ANOMALY": 255.3411,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 22076,
"ELEMENT_SET_NO": 999,
"REV_AT_EPOCH": 60192,
"BSTAR": 0.00014508984,
"MEAN_MOTION_DOT": -2.8e-7,
"MEAN_MOTION_DDOT": 0
}