RU | EN | ZH --:-- UTC Sign in

SITRO-AIS-55

In orbit NORAD 59809 DAYJ-0946-5871-8218-4145 Russia

Time in UTC

—

No observations scheduled

82

Observations over 30 days

77%

Successful observations

4k

Frames, latest 2026-10-11 01:43 UTC

Mission information
Spacecraft name
SITRO-AIS-55
Other names
SC2343
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
2024-05-16 00:00:00
Separation time
2024-05-16 00:00:00
Last observers
Observer
Time of receipt
2026-10-11 01:43:04 UTC
2026-10-11 00:10:08 UTC
2026-10-10 22:33:52 UTC
2026-10-10 16:33:51 UTC
2026-10-10 15:04:22 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
436.74 km
Apogee
446.69 km
Inclination
97.7°
Period
93.5 min
Semi-major axis
6819.8 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-09 12:46:40 UTC
Two-line elements (TLE)
1 59809U 24092K   26282.17545692  .00019164  00000-0  47438-3 0  9997
2 59809 97.6711 60.1023 0007298 102.8252 257.3810 15.40455883132760
Copy content
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 08:30:20 STARLINK-3155
NORAD 49739
OBJECT K
NORAD 59809
1.113 14.74 4.5e-05
2026-10-11 09:17:06 STARLINK-3155
NORAD 49739
OBJECT K
NORAD 59809
4.784 14.75 2.4e-06
2026-10-11 21:33:05 OBJECT K
NORAD 59809
HULIANWANG JISHU SHIYAN 10C
NORAD 69322
3.854 14.65 1.3e-07
2026-10-14 23:21:16 JILIN-1 GAOFEN 2A
NORAD 44777
OBJECT K
NORAD 59809
4.699 6.58 1.8e-07
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 11:54:21 STARLINK-5330
NORAD 55282
OBJECT K
NORAD 59809
3.563 14.40 4.8e-06
2026-10-15 13:27:51 STARLINK-5330
NORAD 55282
OBJECT K
NORAD 59809
4.777 14.39 2.7e-06
2026-10-15 15:43:22 OBJECT K
NORAD 59809
FLOCK 4G-18
NORAD 62680
3.610 7.13 3.0e-07
2026-10-17 01:16:47 OBJECT K
NORAD 59809
SL-3 R/B
NORAD 14208
4.746 13.43 3.0e-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