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ZORKIY-2M

In orbit NORAD 57177 AMWD-8238-3001-8498-3030 Спутникс Russia

Time in UTC

—

No observations scheduled

21

Observations over 30 days

95%

Successful observations

17k

Frames, latest 2026-10-10 18:31 UTC

Mission information
Spacecraft name
ZORKIY-2M
Other names
SXC12−222
Call sign
-
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2023-06-28 11:34:00
Separation time
Last observers
Observer
Time of receipt
2026-10-10 18:31:01 UTC
2026-10-10 09:16:05 UTC
2026-10-06 18:19:23 UTC
2026-10-06 07:29:33 UTC
2026-10-02 10:24:39 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
486.52 km
Apogee
506.27 km
Inclination
97.5°
Period
94.6 min
Semi-major axis
6874.5 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:48 UTC
Two-line elements (TLE)
1 57177U 23091M   26283.29992948  .00006124  00000-0  26957-3 0  9990
2 57177 97.4962 341.9167 0014360 77.0178 283.2661 15.22125716181506
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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
2026-10-12 10:52:38 ZORKIY-2M 1
NORAD 57177
RASSVET-3 31
NORAD 100097
2.842 14.82 2.1e-07
2026-10-13 09:44:31 ZORKIY-2M 1
NORAD 57177
AE5RB
NORAD 66693
1.400 1.84 2.2e-06
2026-10-13 23:10:17 QB50P1
NORAD 40025
ZORKIY-2M 1
NORAD 57177
4.906 5.02 1.7e-07
2026-10-13 23:11:43 ZORKIY-2M 1
NORAD 57177
PESSOA
NORAD 100139
2.252 11.66 6.0e-07
2026-10-15 18:21:22 ZORKIY-2M 1
NORAD 57177
HULIANWANG JISHU SHIYAN 10B
NORAD 69321
2.426 14.02 3.7e-07
2026-10-15 18:33:13 ZORKIY-2M 1
NORAD 57177
FENGYUN 1C DEB
NORAD 29868
0.911 1.50 5.3e-06
2026-10-16 06:02:21 CELTEE 1
NORAD 41850
ZORKIY-2M 1
NORAD 57177
2.486 15.06 2.6e-07
2026-10-16 17:23:25 ZORKIY-2M 1
NORAD 57177
RASSVET-3 2
NORAD 68361
4.744 11.83 1.3e-07
2026-10-17 01:18:00 CARTOSAT-2D
NORAD 41948
ZORKIY-2M 1
NORAD 57177
1.729 0.21 1.5e-06
2026-10-17 01:36:56 ZORKIY-2M 1
NORAD 57177
GITAI-SC1
NORAD 62388
4.608 7.21 1.9e-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