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

CSTP-3.1

In orbit NORAD 67278 SSIE-2783-1620-5714-5787 СТЦ Russia

Soyuz 2.1b Fregat-M

Carrier rocket

Cosmodrome Site 1S

Spaceport

77

Observations all time

Mission information
Spacecraft name
CSTP-3.1
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
2026-01-29 17:48:53 UTC
Satellite appearance
Operator
СТЦ
Data for the last 30 days
Orbital parameters of the satellite
Perigee
482.80 km
Apogee
500.58 km
Inclination
97.4°
Period
94.5 min
Semi-major axis
6869.8 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:42 UTC
Two-line elements (TLE)
1 67278U 25313AG  26285.15653386  .00007786  00000-0  32646-3 0  9996
2 67278 97.3796 357.7906 0012853 321.6644 38.3679 15.23702933 43766
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
2026-10-13 12:47:58 OBJECT AG
NORAD 67278
EDDA-1
NORAD 69017
1.550 15.11 6.5e-07
2026-10-14 14:25:17 SITRO-AIS-60
NORAD 67260
OBJECT AG
NORAD 67278
0.997 0.00 3.7e-05
2026-10-14 15:03:57 SITRO-AIS-60
NORAD 67260
OBJECT AG
NORAD 67278
0.344 0.00 3.7e-05
2026-10-14 19:18:17 OBJECT AG
NORAD 67278
LANDSAT 5
NORAD 14780
3.624 14.53 9.0e-07
2026-10-15 01:36:47 OBJECT AG
NORAD 67278
COSMOS 2251 DEB
NORAD 34449
4.076 14.97 9.9e-08
2026-10-15 03:51:00 T1DES 1 (DRAGOON 1)
NORAD 64542
OBJECT AG
NORAD 67278
4.339 5.62 2.2e-07
2026-10-15 07:47:54 SITRO-AIS-65
NORAD 67266
OBJECT AG
NORAD 67278
4.633 0.07 2.1e-07
2026-10-15 11:54:15 STARLINK-3566
NORAD 51880
OBJECT AG
NORAD 67278
0.927 11.19 1.1e-04
2026-10-15 19:10:48 OBJECT AG
NORAD 67278
GEN1A-1
NORAD 69004
0.788 15.09 2.5e-06
2026-10-16 09:04:15 OBJECT AG
NORAD 67278
IRIDE-MS1-EAGLET 2-13
NORAD 68450
2.088 12.76 6.2e-07
2026-10-16 13:08:19 STARLINK-6190
NORAD 56774
OBJECT AG
NORAD 67278
3.386 14.99 4.3e-06
2026-10-17 23:28:37 STARLINK-4473
NORAD 53660
OBJECT AG
NORAD 67278
2.772 14.86 6.8e-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