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COSMOS 2581

In orbit NORAD 62902 SXZZ-8618-6501-9985-3341 Russia

2025

Launch

0

Observations all time

Mission information
Spacecraft name
COSMOS 2581
Other names
2025-026A
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2025-02-05 00:00:00
Separation time
2025-02-05 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
571.14 km
Apogee
586.32 km
Inclination
82.0°
Period
96.3 min
Semi-major axis
6956.9 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:58 UTC
Two-line elements (TLE)
1 62902U 25026A   26283.73579074  .00001097  00000-0  97547-4 0  9990
2 62902 81.9948 316.5778 0010907 40.4209 319.7819 14.95215869 91483
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-11 23:28:21 COSMOS 2581
NORAD 62902
SHIYAN-30 01
NORAD 65851
3.679 6.86 2.9e-07
2026-10-12 00:34:48 GRUS-1B
NORAD 47934
COSMOS 2581
NORAD 62902
4.176 14.67 1.0e-07
2026-10-12 01:23:37 COSMOS 2581
NORAD 62902
LEMUR-2-ELEONORE
NORAD 69940
4.137 13.78 1.3e-07
2026-10-12 03:47:51 COSMOS 2581
NORAD 62902
UVSQ-SAT NG
NORAD 63251
2.528 14.29 3.2e-07
2026-10-12 05:24:12 COSMOS 2581
NORAD 62902
UVSQ-SAT NG
NORAD 63251
4.355 14.28 1.1e-07
2026-10-12 09:59:00 STARLINK-6040
NORAD 56809
COSMOS 2581
NORAD 62902
2.469 14.41 9.7e-06
2026-10-12 23:48:26 COSMOS 2581
NORAD 62902
TURKSAT-3USAT
NORAD 39152
2.233 7.98 7.7e-07
2026-10-13 17:35:25 COSMOS 2581
NORAD 62902
FENGYUN 1C DEB
NORAD 31296
4.063 8.48 2.3e-07
2026-10-13 19:57:27 COSMOS 2581
NORAD 62902
FENGYUN 1C DEB
NORAD 30716
2.487 14.96 2.6e-07
2026-10-14 11:43:33 COSMOS 2581
NORAD 62902
OKEAN-4
NORAD 23317
2.835 14.98 2.6e-06
2026-10-15 00:35:56 STARLINK-6059
NORAD 56814
COSMOS 2581
NORAD 62902
1.849 14.50 1.7e-05
2026-10-15 03:50:33 COSMOS 2581
NORAD 62902
STARLINK-34669
NORAD 64811
4.950 2.12 5.4e-06
2026-10-15 06:28:53 SITRO-AIS 22
NORAD 61740
COSMOS 2581
NORAD 62902
2.873 15.00 1.9e-07
2026-10-15 07:16:59 SITRO-AIS 22
NORAD 61740
COSMOS 2581
NORAD 62902
4.731 15.05 6.9e-08
2026-10-15 08:05:13 SITRO-AIS 22
NORAD 61740
COSMOS 2581
NORAD 62902
3.746 15.00 1.1e-07
2026-10-15 12:02:04 COSMOS 2581
NORAD 62902
CZ-4C DEB
NORAD 44616
1.920 7.92 1.0e-06
2026-10-15 15:19:18 COSMOS 2581
NORAD 62902
NOAA 16 DEB
NORAD 41140
3.977 14.81 1.1e-07
2026-10-15 16:56:37 COSMOS 2581
NORAD 62902
IRIDIUM 33 DEB
NORAD 34091
4.134 3.63 2.5e-07
2026-10-16 13:41:51 STARLINK-6204
NORAD 56488
COSMOS 2581
NORAD 62902
3.233 5.58 1.2e-05
2026-10-16 21:47:19 COSMOS 2581
NORAD 62902
AE2A
NORAD 64591
4.283 11.19 1.7e-07
2026-10-17 05:42:22 COSMOS 2581
NORAD 62902
STARLINK-36202
NORAD 67094
3.475 13.56 5.9e-06
2026-10-17 08:56:19 STARLINK-5284
NORAD 55297
COSMOS 2581
NORAD 62902
4.288 13.02 4.3e-06
2026-10-17 09:04:43 COSMOS 2581
NORAD 62902
CZ-6A DEB
NORAD 61166
2.695 7.56 5.4e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite