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

InnoSat3

In orbit NORAD 64894 VCOU-5138-4852-6587-2660 Геоскан Russia

Time in UTC

13.10 00:39

Scheduled · Великий Устюг

1797

Observations over 30 days

72%

Successful observations

1M

Frames, latest 2026-10-12 16:59 UTC

Mission information
Spacecraft name
InnoSat3
Other names
ИнноСат3, RS92S0
Call sign
RS92S0
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
2025-07-25 05:54:00
Separation time
Last observers
Observer
Time of receipt
2026-10-12 16:59:41 UTC
2026-10-12 13:42:28 UTC
2026-10-12 13:39:57 UTC
2026-10-12 13:42:04 UTC
2026-10-12 13:41:48 UTC
Satellite appearance
Operator
Orbital parameters of the satellite
Perigee
399.86 km
Apogee
410.22 km
Inclination
97.5°
Period
92.7 min
Semi-major axis
6782.8 km
Velocity
7.67 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:41 UTC
Two-line elements (TLE)
1 64894U 25155U   26285.30031489  .00052427  00000-0  83440-3 0  9992
2 64894 97.4622 260.4560 0007642 107.7435 252.4652 15.53092748 99088
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
2026-10-15 03:47:30 STARLINK-1446
NORAD 45663
INNOSAT 3 (RS92S0)
NORAD 64894
4.636 13.38 3.5e-06
2026-10-15 05:51:33 INNOSAT 3 (RS92S0)
NORAD 64894
STARLINK-38170
NORAD 100636
4.592 11.44 4.5e-06
2026-10-15 11:23:57 INNOSAT 3 (RS92S0)
NORAD 64894
SL-8 R/B
NORAD 12139
4.931 15.40 3.0e-07
2026-10-17 07:26:48 INNOSAT 3 (RS92S0)
NORAD 64894
CZ-4 DEB
NORAD 35381
4.401 10.80 1.7e-07
2026-10-17 18:25:01 STARLINK-1762
NORAD 46342
INNOSAT 3 (RS92S0)
NORAD 64894
4.822 13.95 2.9e-06

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