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Geoscan-3

In orbit NORAD 64893 NAYK-9396-4687-3348-2272 Геоскан Russia

Time in UTC

03:11

Next pass · Чукотка · 28°

11.10 03:21

Scheduled · Мурманск

1549

Observations over 30 days

67%

Successful observations

338k

Frames, latest 2026-10-11 02:00 UTC

Mission information
Spacecraft name
Geoscan-3
Other names
Геоскан-3, RS92S3
Call sign
RS92S3
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
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
440.47 km
Apogee
451.02 km
Inclination
97.5°
Period
93.6 min
Semi-major axis
6823.8 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:59 UTC
Two-line elements (TLE)
1 64893U 25155T   26283.60322765  .00021321  00000-0  55113-3 0  9997
2 64893 97.4677 255.2336 0007754 116.9506 243.2532 15.39101833 98584
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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 04:57:30 STARLINK-4434
NORAD 53501
GEOSCAN 3 (RS92S3)
NORAD 64893
4.963 14.79 2.2e-06
2026-10-14 22:31:56 OBJECT AL
NORAD 57038
GEOSCAN 3 (RS92S3)
NORAD 64893
2.467 14.34 3.4e-07
2026-10-15 04:43:38 STARLINK-4448
NORAD 53504
GEOSCAN 3 (RS92S3)
NORAD 64893
3.584 14.80 4.2e-06
2026-10-15 05:59:23 SHERPA-AC1
NORAD 52763
GEOSCAN 3 (RS92S3)
NORAD 64893
1.245 15.15 1.0e-06
2026-10-16 16:46:26 HERMES-3
NORAD 63835
GEOSCAN 3 (RS92S3)
NORAD 64893
4.314 9.31 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