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FOSSASAT-2E25

In orbit NORAD 68478 OXYP-6047-8317-6002-4754 Spain

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

17

Observations all time

Mission information
Spacecraft name
FOSSASAT-2E25
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 4E
Launch time
2026-03-30 11:02:00
Separation time
Last observers
Observer
Time of receipt
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
587.50 km
Apogee
587.99 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6965.9 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-09 04:46:17 UTC
Two-line elements (TLE)
1 68478U 26067BQ  26281.82417343  .00001354  00000-0  13808-3 0  9991
2 68478 97.7741 238.5113 0000353 281.8301 78.2878 14.92312808 28678
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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
2026-10-11 22:11:26 FOSSASAT-2E25
NORAD 68478
PEGASUS DEB
NORAD 24602
4.555 14.83 8.9e-08
2026-10-11 22:57:25 LEAP-1
NORAD 65321
FOSSASAT-2E25
NORAD 68478
2.914 12.65 3.2e-07
2026-10-11 23:45:43 LEAP-1
NORAD 65321
FOSSASAT-2E25
NORAD 68478
0.691 12.68 5.7e-06
2026-10-12 19:08:36 FOSSASAT-2E25
NORAD 68478
ESSAIM-2
NORAD 28495
4.618 5.70 1.9e-07
2026-10-13 15:55:40 FOSSASAT-2E25
NORAD 68478
CZ-4B DEB
NORAD 26262
4.568 14.44 9.3e-08
2026-10-15 02:34:14 FOSSASAT-2E25
NORAD 68478
CZ-6A DEB
NORAD 55190
4.307 13.45 1.3e-07
2026-10-15 18:46:44 FOSSASAT-2E25
NORAD 68478
GSLV R/B
NORAD 54149
4.116 14.66 1.0e-07
2026-10-16 01:59:49 FOSSASAT-2E25
NORAD 68478
BALKAN-3
NORAD 69903
4.843 7.26 1.7e-07
2026-10-16 02:48:06 FOSSASAT-2E25
NORAD 68478
BALKAN-3
NORAD 69903
4.982 7.24 1.6e-07
2026-10-16 04:25:58 FOSSASAT-2E25
NORAD 68478
FENGYUN 1C DEB
NORAD 31715
1.446 10.57 1.6e-06
2026-10-17 03:38:40 FOSSASAT-2E25
NORAD 68478
CZ-6A DEB
NORAD 56588
2.266 13.72 4.5e-07
2026-10-17 08:07:38 FOSSASAT-2E25
NORAD 68478
H-2A DEB
NORAD 38347
4.528 14.98 7.7e-08
2026-10-17 10:08:13 YAOGAN-3
NORAD 32289
FOSSASAT-2E25
NORAD 68478
4.651 8.82 1.7e-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