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Grifon-3

In orbit NORAD 67280 RTQY-5459-1602-5776-1173 ОКБ5 Russia

Soyuz 2.1b Fregat-M

Carrier rocket

Cosmodrome Site 1S

Spaceport

22

Observations all time

Mission information
Spacecraft name
Grifon-3
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2025-12-28 13:18:05
Separation time
Last observers
Observer
Time of receipt
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
484.67 km
Apogee
500.61 km
Inclination
97.4°
Period
94.5 min
Semi-major axis
6870.7 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 22:09:14 UTC
Two-line elements (TLE)
1 67280U 25313AJ  26286.48037340  .00004982  00000-0  21210-3 0  9992
2 67280 97.3892 359.4183 0011511 310.2687 49.7543 15.23383504 43959
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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
2026-10-14 02:56:30 OBJECT P
NORAD 64889
OBJECT AJ
NORAD 67280
3.163 11.97 3.0e-07
2026-10-14 05:36:48 OBJECT AJ
NORAD 67280
SELENE
NORAD 69020
4.370 15.09 8.2e-08
2026-10-14 07:11:28 OBJECT AJ
NORAD 67280
SELENE
NORAD 69020
4.715 15.09 7.1e-08
2026-10-14 18:46:11 COSMOS 2579
NORAD 61730
OBJECT AJ
NORAD 67280
4.396 14.49 1.0e-07
2026-10-14 19:39:23 SPACEMOBILE-006
NORAD 67232
OBJECT AJ
NORAD 67280
1.907 14.07 6.0e-07
2026-10-15 05:04:34 OBJECT AJ
NORAD 67280
IRIDIUM 33 DEB
NORAD 46971
3.924 15.20 9.7e-08
2026-10-15 09:59:26 OBJECT AJ
NORAD 67280
HYDRA-3
NORAD 69022
2.487 15.09 2.5e-07
2026-10-15 13:41:38 OBJECT AJ
NORAD 67280
OBJECT AS
NORAD 67288
1.919 0.01 1.2e-06
2026-10-15 14:21:19 OBJECT AJ
NORAD 67280
OBJECT AS
NORAD 67288
2.728 0.00 1.2e-06
2026-10-16 19:06:37 YAOGAN-39 05A
NORAD 58557
OBJECT AJ
NORAD 67280
4.044 7.95 2.3e-07
2026-10-17 14:26:52 SIGI
NORAD 62632
OBJECT AJ
NORAD 67280
3.555 0.78 3.5e-07
2026-10-17 15:19:50 STARLINK-5917
NORAD 55942
OBJECT AJ
NORAD 67280
2.135 10.08 2.3e-05
2026-10-17 16:01:34 SITRO-AIS 28
NORAD 59071
OBJECT AJ
NORAD 67280
2.565 5.70 6.3e-07
2026-10-18 05:25:41 ACCENTURE-1
NORAD 66767
OBJECT AJ
NORAD 67280
0.825 0.18 6.5e-06
2026-10-18 07:12:03 STARLINK-4478
NORAD 53529
OBJECT AJ
NORAD 67280
3.377 14.01 5.8e-06
2026-10-19 10:42:25 OBJECT AJ
NORAD 67280
JIELONG-3 R/B
NORAD 58507
2.869 15.17 1.8e-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