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SITRO-AIS-46

In orbit NORAD 61774 ZBVE-3642-7824-0324-5322 Спутникс

Time in UTC

08:40

Next pass · ИТ-куб, Калининград · 13°

—

No observations scheduled

1

Observations over 30 days

80%

Successful observations

529

Frames, latest 2026-09-15 06:08 UTC

Mission information
Spacecraft name
SITRO-AIS-46
Other names
SC2334
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
2024-11-04 23:18:40
Separation time
Last observers
Observer
Time of receipt
2026-09-15 06:08:02 UTC
2026-09-05 06:07:10 UTC
2025-03-18 06:12:34 UTC
2025-01-11 18:57:16 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
331.50 km
Apogee
337.85 km
Inclination
97.3°
Period
91.3 min
Semi-major axis
6712.0 km
Velocity
7.69 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:03 UTC
Two-line elements (TLE)
1 61774U 24199AR  26286.91065731  .00153391  00000-0  90604-3 0  9990
2 61774 97.2611 167.7701 0004878 153.8683 206.2831 15.77682950153071
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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
2026-10-15 11:25:23 SITRO-AIS 46
NORAD 61774
ARC-1
NORAD 40969
4.084 12.58 1.7e-07
2026-10-16 04:06:38 STARLINK-2033
NORAD 47650
SITRO-AIS 46
NORAD 61774
4.519 11.42 4.7e-06
2026-10-16 05:37:57 STARLINK-2033
NORAD 47650
SITRO-AIS 46
NORAD 61774
4.347 11.45 5.0e-06
2026-10-16 09:26:16 STARLINK-2033
NORAD 47650
SITRO-AIS 46
NORAD 61774
1.918 11.54 2.6e-05
2026-10-17 18:13:25 SITRO-AIS 46
NORAD 61774
STARLINK-38088
NORAD 100114
3.602 14.27 5.0e-06
2026-10-17 20:20:18 STARLINK-1304
NORAD 45376
SITRO-AIS 46
NORAD 61774
4.671 6.92 5.5e-06
2026-10-17 20:30:22 SITRO-AIS 46
NORAD 61774
STARLINK-38088
NORAD 100114
2.106 14.31 1.5e-05
2026-10-19 03:36:51 SITRO-AIS 46
NORAD 61774
STARLINK-38010
NORAD 69727
4.297 15.03 9.3e-08
2026-10-19 05:53:48 SITRO-AIS 46
NORAD 61774
STARLINK-38010
NORAD 69727
4.716 15.06 7.7e-08

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