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METEOR M2-4

In orbit NORAD 59051 VSVI-4798-5613-4587-2414 Роскосмос Russia

Observations 8392
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Time in UTC

06:04

Next pass · Восточное, Хабаровский край

11.10 06:05

Scheduled · МАН РС(Я) ГЕОСКАН УКВ

384

Observations over 30 days

74%

Successful observations

12k

Frames, latest 2026-10-10 22:05 UTC

Mission information
Spacecraft name
METEOR M2-4
Other names
METEOR 2 2-4, METEOR-M N2-4
Status
Active
The satellite is in orbit
Launch and timeline
Launch
Soyuz 2.1b/Fregat-M | Meteor-M No.2-4 & others
Carrier rocket
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2024-02-29 05:43:26
Separation time
Last observers
Observer
Time of receipt
МАН РС(Я) ГЕОСКАН УКВ-PP41qp
2026-10-10 22:05:01 UTC
МАН РС(Я) ГЕОСКАН УКВ-PP41qp
2026-10-10 20:25:10 UTC
МАН РС(Я) ГЕОСКАН УКВ-PP41qp
2026-10-10 18:47:37 UTC
МАН РС(Я) ГЕОСКАН УКВ-PP41qp
2026-10-10 17:01:46 UTC
Обозерский-LP03dl
2026-10-10 11:42:27 UTC
Satellite appearance
Operator
Роскосмос
Data for the last 30 days
Orbital parameters of the satellite
Perigee
809.42 km
Apogee
819.12 km
Inclination
98.7°
Period
101.2 min
Semi-major axis
7192.4 km
Velocity
7.43 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:38 UTC
Two-line elements (TLE)
1 59051U 24039A   26283.96590608  .00000016  00000-0  27068-4 0  9996
2 59051  98.7176 241.8858 0006741 186.3144 173.7950 14.22439707135720
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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 18:28:10 METEOR-M2 4
NORAD 59051 		CZ-6A DEB
NORAD 60791 		4.750 1.44 1.9e-07
2026-10-11 20:40:38 METEOR-M2 4
NORAD 59051 		CZ-6A DEB
NORAD 54473 		4.075 8.20 2.3e-07
2026-10-12 00:14:55 METEOR-M2 4
NORAD 59051 		CZ-6A DEB
NORAD 61178 		4.375 2.14 2.3e-07
2026-10-12 05:57:49 METEOR-M2 4
NORAD 59051 		DELTA 1 DEB
NORAD 37662 		3.109 7.92 4.0e-07
2026-10-12 19:26:55 METEOR-M2 4
NORAD 59051 		METOP-SGA1
NORAD 65159 		4.438 11.26 1.6e-07
2026-10-12 22:49:16 METEOR-M2 4
NORAD 59051 		METEOR 1-17 DEB
NORAD 57543 		4.854 9.34 1.5e-07
2026-10-13 00:30:34 METEOR-M2 4
NORAD 59051 		METEOR 1-17 DEB
NORAD 57543 		3.882 9.35 2.4e-07
2026-10-13 01:28:17 METEOR-M2 4
NORAD 59051 		FENGYUN 1C DEB
NORAD 31368 		4.399 12.47 1.4e-07
2026-10-13 02:11:52 METEOR-M2 4
NORAD 59051 		METEOR 1-17 DEB
NORAD 57543 		3.198 9.37 3.5e-07
2026-10-13 03:53:10 METEOR-M2 4
NORAD 59051 		METEOR 1-17 DEB
NORAD 57543 		2.992 9.38 4.0e-07
2026-10-13 05:34:28 METEOR-M2 4
NORAD 59051 		METEOR 1-17 DEB
NORAD 57543 		3.344 9.39 3.2e-07
2026-10-13 07:15:46 METEOR-M2 4
NORAD 59051 		METEOR 1-17 DEB
NORAD 57543 		4.105 9.41 2.1e-07
2026-10-13 11:17:45 METEOR-M2 4
NORAD 59051 		COSMOS 2251 DEB
NORAD 34413 		4.683 14.81 6.9e-08
2026-10-13 11:33:27 METEOR-M2 4
NORAD 59051 		IONOSFERA-M 3
NORAD 64876 		2.967 0.14 5.0e-07
2026-10-13 12:24:07 METEOR-M2 4
NORAD 59051 		IONOSFERA-M 3
NORAD 64876 		4.135 0.14 2.6e-07
2026-10-13 12:58:45 METEOR-M2 4
NORAD 59051 		COSMOS 2251 DEB
NORAD 34413 		2.500 14.81 2.4e-07
2026-10-13 14:39:45 METEOR-M2 4
NORAD 59051 		COSMOS 2251 DEB
NORAD 34413 		3.128 14.82 1.5e-07
2026-10-13 16:20:45 METEOR-M2 4
NORAD 59051 		COSMOS 2251 DEB
NORAD 34413 		4.912 14.82 6.2e-08
2026-10-13 20:46:39 METEOR-M2 4
NORAD 59051 		DMSP 5D-2 F14 DEB
NORAD 62939 		2.770 10.59 4.3e-07
2026-10-14 10:18:53 METEOR-M2 4
NORAD 59051 		CZ-6A DEB
NORAD 54320 		3.701 1.33 3.2e-07
2026-10-14 14:20:05 EXACTVIEW-1 (ADS-1B)
NORAD 38709 		METEOR-M2 4
NORAD 59051 		3.806 14.52 1.2e-07
2026-10-14 14:31:35 METEOR-M2 4
NORAD 59051 		DTUSAT
NORAD 27842 		4.299 6.11 2.2e-07
2026-10-14 15:19:16 METEOR-M2 4
NORAD 59051 		FENGYUN 1C DEB
NORAD 33682 		2.039 12.53 6.5e-07
2026-10-14 17:52:32 METEOR-M2 4
NORAD 59051 		FENGYUN 1C DEB
NORAD 30138 		1.343 11.00 1.8e-06
2026-10-14 21:17:54 METEOR-M2 4
NORAD 59051 		SL-3 R/B
NORAD 12457 		3.597 14.88 3.1e-07
2026-10-14 23:04:11 METEOR-M2 4
NORAD 59051 		SCOUT D-1 R/B
NORAD 7228 		4.079 13.42 1.9e-07
2026-10-15 07:31:29 METEOR-M2 4
NORAD 59051 		SL-16 R/B
NORAD 19120 		3.104 9.71 4.9e-06
2026-10-16 15:23:07 METEOR-M2 4
NORAD 59051 		CZ-2C R/B
NORAD 31114 		3.602 14.01 1.6e-07
2026-10-16 21:22:15 METEOR-M2 4
NORAD 59051 		FENGYUN 1C DEB
NORAD 31429 		4.587 10.54 1.6e-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