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CEVROSAT-1

In orbit NORAD 66308 OKGA-8851-7796-3537-9901 Czechia

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 40

Spaceport

127

Observations all time

Mission information
Spacecraft name
CEVROSAT-1
Other names
OK0CVR
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
Falcon 9 Block 5
Spaceport
Space Launch Complex 40
Launch time
2025-11-02 06:09:00
Separation time
2025-11-02 07:18:30
Last observers
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
500.20 km
Apogee
506.54 km
Inclination
45.4°
Period
94.7 min
Semi-major axis
6881.5 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-09 12:46:41 UTC
Two-line elements (TLE)
1 66308U 25248R   26282.25880649  .00003898  00000-0  18342-3 0  9995
2 66308 45.3969 229.1130 0004612 307.2380 52.8086 15.21328416 51889
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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
2026-10-10 23:39:33 OBJECT T
NORAD 57183
TOMORROW-S8
NORAD 66308
2.937 13.04 3.0e-07
2026-10-11 16:16:28 SCS-01 L
NORAD 63992
TOMORROW-S8
NORAD 66308
3.402 13.71 2.0e-07
2026-10-11 17:51:08 SCS-01 L
NORAD 63992
TOMORROW-S8
NORAD 66308
2.149 13.72 5.0e-07
2026-10-11 19:25:48 SCS-01 L
NORAD 63992
TOMORROW-S8
NORAD 66308
3.027 13.73 2.5e-07
2026-10-11 19:53:30 YAOGAN-39 02A
NORAD 57886
TOMORROW-S8
NORAD 66308
4.676 2.76 2.0e-07
2026-10-12 00:08:39 TOMORROW-S8
NORAD 66308
CZ-4C R/B
NORAD 49123
3.448 9.04 3.1e-07
2026-10-12 00:57:07 SCS-01 L
NORAD 63992
TOMORROW-S8
NORAD 66308
3.866 13.79 1.5e-07
2026-10-12 02:32:15 TOMORROW-S8
NORAD 66308
FLOCK 4H-9
NORAD 66712
2.734 13.86 3.0e-07
2026-10-12 06:44:59 GHGSAT-C12
NORAD 64529
TOMORROW-S8
NORAD 66308
4.122 14.42 1.2e-07
2026-10-13 07:44:00 TOMORROW-S8
NORAD 66308
FLOCK 4H-20
NORAD 66723
2.574 14.08 3.3e-07
2026-10-13 18:47:01 TOMORROW-S8
NORAD 66308
OBJECT AC
NORAD 67274
2.902 14.15 2.5e-07
2026-10-14 06:36:18 SCS-01 F
NORAD 63987
TOMORROW-S8
NORAD 66308
3.477 14.16 1.8e-07
2026-10-14 10:33:56 TOMORROW-S8
NORAD 66308
IHI-SAT2
NORAD 66772
3.986 14.23 1.3e-07
2026-10-14 11:21:16 TOMORROW-S8
NORAD 66308
IHI-SAT2
NORAD 66772
4.162 14.24 1.2e-07
2026-10-14 17:19:37 PROPCUBE 3
NORAD 40973
TOMORROW-S8
NORAD 66308
4.164 4.84 2.4e-07
2026-10-14 19:15:47 TOMORROW-S8
NORAD 66308
SHIYAN-33
NORAD 68405
1.686 14.31 7.2e-07
2026-10-14 22:25:05 TRANSPORTER-13 OBJECT M
NORAD 63221
TOMORROW-S8
NORAD 66308
4.917 7.06 1.6e-07
2026-10-16 07:03:31 WORLDVIEW-1 (WV-1)
NORAD 32060
TOMORROW-S8
NORAD 66308
2.560 13.89 3.4e-07
2026-10-16 08:06:13 STARLINK-4346
NORAD 53073
TOMORROW-S8
NORAD 66308
4.251 9.93 5.8e-06
2026-10-16 09:04:12 PEXT (BARD)
NORAD 64874
TOMORROW-S8
NORAD 66308
4.404 14.28 1.1e-07
2026-10-16 22:19:54 SJ-7
NORAD 28737
TOMORROW-S8
NORAD 66308
4.911 13.60 9.9e-08

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