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

Marafon

In orbit NORAD 67250 PBIL-7523-6013-0175-4680 Роскосмос Russia

Time in UTC

00:20

Next pass · МАН РС(Я) ГЕОСКАН УКВ · 16°

—

No observations scheduled

5

Observations over 30 days

0%

Successful observations

0

Frames received

Mission information
Spacecraft name
Marafon
Other names
ОО Марафон, Test Model Maradon
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
Satellite appearance
Operator
Роскосмос
Data for the last 30 days
Orbital parameters of the satellite
Perigee
492.20 km
Apogee
694.65 km
Inclination
97.6°
Period
96.6 min
Semi-major axis
6971.5 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 22:09:14 UTC
Two-line elements (TLE)
1 67250U 25313C   26286.45656318  .00008875  00000-0  74853-3 0  9994
2 67250 97.6060 352.7974 0144999 304.0820 54.6707 14.90511688 42963
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
2026-10-14 01:18:31 OBJECT C
NORAD 67250
JACKAL-004
NORAD 69012
4.019 15.07 1.0e-07
2026-10-14 21:59:56 OBJECT AK
NORAD 57037
OBJECT C
NORAD 67250
4.697 4.91 1.9e-07
2026-10-15 11:29:21 KUIPER-00013
NORAD 63729
OBJECT C
NORAD 67250
4.494 13.76 1.1e-07
2026-10-16 02:21:41 ITUPSAT1
NORAD 35935
OBJECT C
NORAD 67250
2.806 14.54 2.2e-07
2026-10-16 03:49:04 OBJECT C
NORAD 67250
CZ-6A DEB
NORAD 61322
4.111 12.43 1.6e-07
2026-10-16 05:25:58 OBJECT C
NORAD 67250
SARA
NORAD 21578
4.041 2.67 1.1e-07
2026-10-16 09:27:41 MICE-1
NORAD 66684
OBJECT C
NORAD 67250
2.523 0.71 6.9e-07
2026-10-17 16:55:20 OBJECT C
NORAD 67250
UNKNOWN
NORAD 87239
4.199 14.96 8.4e-08
2026-10-18 08:29:26 OBJECT C
NORAD 67250
KUIPER-00551
NORAD 69618
4.595 14.61 8.9e-08
2026-10-18 20:39:15 KUIPER-00245
NORAD 67150
OBJECT C
NORAD 67250
1.956 14.54 4.8e-07
2026-10-19 01:54:16 PHI 1
NORAD 66775
OBJECT C
NORAD 67250
2.655 0.76 6.2e-07
2026-10-19 07:55:53 KUIPER-00265
NORAD 67159
OBJECT C
NORAD 67250
2.882 14.54 2.2e-07
2026-10-19 09:04:23 OBJECT C
NORAD 67250
COSMOS 2251 DEB
NORAD 34819
2.522 11.21 4.9e-07
2026-10-19 17:02:35 OBJECT C
NORAD 67250
RUBIN-3 & SL-8 R/B
NORAD 27561
4.227 14.57 1.0e-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