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SITRO-AIS-11

In orbit NORAD 57208 BTMY-6498-5817-1415-4137 Спутникс Russia

Time in UTC

—

No observations scheduled

1

Observations over 30 days

58%

Successful observations

1k

Frames, latest 2026-09-22 21:55 UTC

Mission information
Spacecraft name
SITRO-AIS-11
Other names
Sputnix Smirenny
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Союз-2.1б
Upper stage
Фрегат-М
Spaceport
Восточный
Launch time
2023-06-28 11:34:00
Separation time
Last observers
Observer
Time of receipt
2026-09-17 18:55:41 UTC
2026-06-02 08:14:01 UTC
2025-07-10 19:51:08 UTC
2025-07-07 08:43:58 UTC
2025-07-05 10:54:25 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
430.74 km
Apogee
438.33 km
Inclination
97.5°
Period
93.3 min
Semi-major axis
6812.7 km
Velocity
7.65 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:48 UTC
Two-line elements (TLE)
1 57208U 23091AU  26283.28941767  .00023461  00000-0  53520-3 0  9996
2 57208 97.4985 357.3517 0005577 25.8227 334.3297 15.42886394182515
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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 08:09:24 SITRO-AIS 11 (SHEFFER)
NORAD 57208
LEMUR-2-CAEL
NORAD 58903
4.126 14.20 1.3e-07
2026-10-13 09:50:50 SITRO-AIS 11 (SHEFFER)
NORAD 57208
CZ-4B R/B
NORAD 100657
4.622 10.63 1.6e-07
2026-10-15 06:14:20 STARLINK-4076
NORAD 52667
SITRO-AIS 11 (SHEFFER)
NORAD 57208
4.188 12.93 4.6e-06
2026-10-15 07:01:02 STARLINK-4076
NORAD 52667
SITRO-AIS 11 (SHEFFER)
NORAD 57208
4.842 12.97 3.4e-06
2026-10-15 10:16:14 SITRO-AIS 11 (SHEFFER)
NORAD 57208
OBJECT K
NORAD 59809
4.551 8.04 1.9e-07
2026-10-15 19:27:55 STARLINK-4076
NORAD 52667
SITRO-AIS 11 (SHEFFER)
NORAD 57208
3.087 13.13 8.2e-06
2026-10-15 19:54:22 STARLINK-3716
NORAD 52092
SITRO-AIS 11 (SHEFFER)
NORAD 57208
2.336 14.65 1.0e-05
2026-10-16 09:37:57 JILIN-1 GAOFEN 2A
NORAD 44777
SITRO-AIS 11 (SHEFFER)
NORAD 57208
3.482 1.66 3.6e-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