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Grifon-1

In orbit NORAD 67281 PDBX-0731-2301-4011-4620 ОКБ5 Russia

Soyuz 2.1b Fregat-M

Carrier rocket

Cosmodrome Site 1S

Spaceport

35

Observations all time

Mission information
Spacecraft name
Grifon-1
Other names
Грифон-1
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
2026-01-17 15:03:38 UTC
2026-01-12 18:04:51 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
485.23 km
Apogee
499.45 km
Inclination
97.4°
Period
94.5 min
Semi-major axis
6870.4 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 67281U 25313AK  26286.46223327  .00004654  00000-0  19784-3 0  9992
2 67281 97.3773 359.0065 0010269 309.8077 50.2255 15.23484052 43956
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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 00:44:52 STARLINK-5265
NORAD 55317
OBJECT AK
NORAD 67281
4.987 15.06 1.9e-06
2026-10-15 02:19:22 STARLINK-5265
NORAD 55317
OBJECT AK
NORAD 67281
4.687 15.06 2.2e-06
2026-10-15 10:48:48 STRIX-3
NORAD 59224
OBJECT AK
NORAD 67281
4.274 11.11 1.8e-07
2026-10-15 13:58:48 OBJECT AK
NORAD 67281
ERMIS-2
NORAD 68420
4.021 12.75 1.7e-07
2026-10-15 23:43:46 OBJECT AK
NORAD 67281
BALKAN-2
NORAD 69024
2.738 15.09 2.1e-07
2026-10-16 08:27:46 AEROCUBE 18B
NORAD 63222
OBJECT AK
NORAD 67281
4.383 15.11 8.1e-08
2026-10-16 10:02:17 AEROCUBE 18B
NORAD 63222
OBJECT AK
NORAD 67281
3.412 15.11 1.3e-07
2026-10-16 17:04:22 OBJECT AK
NORAD 67281
CAS500-2
NORAD 69013
3.753 15.10 1.1e-07
2026-10-16 22:14:27 OBJECT AK
NORAD 67281
LOBACHEVSKY (RS83S)
NORAD 67284
0.356 0.04 3.5e-05
2026-10-16 23:01:35 OBJECT AK
NORAD 67281
LOBACHEVSKY (RS83S)
NORAD 67284
3.627 0.04 3.4e-07
2026-10-17 08:49:57 OBJECT AK
NORAD 67281
JEN-1
NORAD 69006
1.126 15.10 1.2e-06
2026-10-17 14:18:59 YAOGAN-35 03B
NORAD 53318
OBJECT AK
NORAD 67281
0.543 13.67 8.0e-06
2026-10-17 14:50:45 OBJECT AK
NORAD 67281
IRIDE-MS1-EAGLET 2-10
NORAD 68451
2.285 12.77 5.2e-07
2026-10-17 19:04:28 OBJECT AK
NORAD 67281
EDDA-1
NORAD 69017
4.638 15.10 7.3e-08
2026-10-18 00:22:19 BISONSAT
NORAD 40974
OBJECT AK
NORAD 67281
4.924 13.87 9.3e-08
2026-10-18 02:10:21 OBJECT AK
NORAD 67281
HELIOS
NORAD 69021
1.950 15.10 4.1e-07
2026-10-18 02:38:05 OBJECT AK
NORAD 67281
RASSVET-3 20
NORAD 100086
4.955 13.74 9.4e-08
2026-10-18 10:24:55 STARLINK-5068
NORAD 55423
OBJECT AK
NORAD 67281
4.981 13.39 3.0e-06
2026-10-18 12:52:08 CARTOSAT-2D
NORAD 41948
OBJECT AK
NORAD 67281
4.895 2.03 1.8e-07
2026-10-18 19:13:07 OBJECT AK
NORAD 67281
SHARJAH-SAT-2
NORAD 68444
4.261 12.75 1.5e-07
2026-10-19 00:19:26 OBJECT AK
NORAD 67281
IRIDIUM 33 DEB
NORAD 46971
2.678 15.22 2.1e-07
2026-10-19 21:17:43 STARLINK-5265
NORAD 55317
OBJECT AK
NORAD 67281
2.228 14.67 1.1e-05

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