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METEOR M2-3

In orbit NORAD 57166 TLCE-8079-2988-7210-7028 Роскосмос Russia

Observations 8398
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Time in UTC

04:33

Next pass · МАН РС(Я) ГЕОСКАН УКВ · 15°

11.10 04:29

Scheduled · МАН РС(Я) ГЕОСКАН УКВ

297

Observations over 30 days

50%

Successful observations

7k

Frames, latest 2026-10-10 18:11 UTC

Mission information
Spacecraft name
METEOR M2-3
Other names
METEOR 2 2-3, METEOR-M N2-3
Status
Active
The satellite is in orbit
Launch and timeline
Launch
Soyuz 2.1b/Fregat-M | Meteor-M No.2-3 & others
Carrier rocket
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2023-06-27 11:34:00
Separation time
Last observers
Observer
Time of receipt
Обозерский-LP03dl
2026-10-10 18:11:36 UTC
Обозерский-LP03dl
2026-10-10 16:40:24 UTC
МАН РС(Я) ГЕОСКАН УКВ-PP41qp
2026-10-10 11:37:28 UTC
МАН РС(Я) ГЕОСКАН УКВ-PP41qp
2026-10-10 09:54:47 UTC
Обозерский-LP03dl
2026-10-10 08:29:35 UTC
Satellite appearance
Operator
Роскосмос
Data for the last 30 days
Orbital parameters of the satellite
Perigee
806.03 km
Apogee
811.61 km
Inclination
98.6°
Period
101.1 min
Semi-major axis
7187.0 km
Velocity
7.44 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:56 UTC
Two-line elements (TLE)
1 57166U 23091A   26283.60933920 -.00000003  00000-0  17547-4 0  9995
2 57166  98.5955 336.1483 0003895 178.4026 181.7166 14.24053845170946
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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 19:41:55 METEOR-M2 3
NORAD 57166 		CZ-6A DEB
NORAD 54458 		3.370 2.97 3.8e-07
2026-10-12 00:45:10 METEOR-M2 3
NORAD 57166 		CZ-6A DEB
NORAD 64636 		3.368 8.71 3.2e-07
2026-10-12 04:58:57 METEOR-M2 3
NORAD 57166 		CZ-6A DEB
NORAD 61079 		2.902 10.71 3.8e-07
2026-10-12 05:47:39 METEOR-M2 3
NORAD 57166 		METEOR 2-8 DEB
NORAD 36326 		3.020 14.85 1.6e-07
2026-10-13 09:40:39 METEOR-M2 3
NORAD 57166 		ARIANE 1 DEB
NORAD 17478 		1.904 7.97 1.1e-06
2026-10-13 20:38:01 METEOR-M2 3
NORAD 57166 		DMSP 5D-2 F13 DEB
NORAD 40487 		1.804 5.50 1.3e-06
2026-10-14 01:40:17 METEOR-M2 3
NORAD 57166 		CZ-6A DEB
NORAD 54532 		0.336 0.87 3.9e-05
2026-10-14 04:11:43 METEOR-M2 3
NORAD 57166 		NOAA 16 DEB
NORAD 42408 		2.257 0.95 8.7e-07
2026-10-14 06:43:31 METEOR-M2 3
NORAD 57166 		NOAA 16 DEB
NORAD 42408 		4.227 0.95 2.5e-07
2026-10-14 07:02:21 METEOR-M2 3
NORAD 57166 		YAOGAN-50 02 DEB
NORAD 100586 		2.781 12.31 3.6e-07
2026-10-15 07:36:47 METEOR-M2 3
NORAD 57166 		FENGYUN 1C DEB
NORAD 31269 		2.324 14.69 2.9e-07
2026-10-15 11:29:05 METEOR-M2 3
NORAD 57166 		FENGYUN 1C DEB
NORAD 32453 		4.097 13.31 1.4e-07
2026-10-16 05:22:53 METEOR-M2 3
NORAD 57166 		FENGYUN 1C DEB
NORAD 31163 		4.316 14.63 8.8e-08
2026-10-16 06:35:46 METEOR-M2 3
NORAD 57166 		FENGYUN 1C DEB
NORAD 30850 		1.787 14.52 5.4e-07
2026-10-16 10:44:18 METEOR-M2 3
NORAD 57166 		SL-16 DEB
NORAD 39849 		1.407 4.23 2.2e-06
2026-10-16 14:41:21 METEOR-M2 3
NORAD 57166 		CZ-12 R/B
NORAD 67531 		3.913 14.22 1.3e-07
2026-10-16 15:16:38 METEOR-M2 3
NORAD 57166 		METEOR 1-17 DEB
NORAD 57537 		4.364 14.86 7.7e-08
2026-10-16 16:57:46 METEOR-M2 3
NORAD 57166 		METEOR 1-17 DEB
NORAD 57537 		1.328 14.86 8.3e-07
2026-10-16 18:38:54 METEOR-M2 3
NORAD 57166 		METEOR 1-17 DEB
NORAD 57537 		1.900 14.86 4.1e-07
2026-10-16 19:25:21 METEOR-M2 3
NORAD 57166 		FENGYUN 1C DEB
NORAD 31259 		4.635 4.43 2.0e-07
2026-10-16 19:31:06 METEOR-M2 3
NORAD 57166 		SL-16 DEB
NORAD 32006 		2.701 12.31 3.8e-07
2026-10-16 20:20:02 METEOR-M2 3
NORAD 57166 		METEOR 1-17 DEB
NORAD 57537 		4.775 14.86 6.5e-08
2026-10-17 01:21:37 METEOR-M2 3
NORAD 57166 		FENGYUN 1C DEB
NORAD 37914 		1.026 5.46 3.9e-06

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