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FOSSASAT-2E26

In orbit NORAD 69899 XLDB-7538-3591-1202-4298

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

13

Observations all time

Mission information
Spacecraft name
FOSSASAT-2E26
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
2026-07-07 07:12:00
Separation time
2026-07-07 08:14:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
587.19 km
Apogee
594.27 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6968.9 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69899U 26156AG  26282.68302829  .00001646  00000-0  17060-3 0  9993
2 69899 97.7415 181.4412 0005076 162.1278 198.0120 14.91354244 14061
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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
2026-10-12 00:52:47 FOSSASAT-2E26
NORAD 69899
CZ-4B DEB
NORAD 26155
0.926 14.97 1.9e-06
2026-10-12 01:25:14 FOSSASAT-2E26
NORAD 69899
FENGYUN 1C DEB
NORAD 30971
4.744 14.95 7.3e-08
2026-10-14 21:23:59 FOSSASAT-2E26
NORAD 69899
CZ-6A DEB
NORAD 56283
3.133 14.79 1.7e-07
2026-10-14 22:01:32 FOSSASAT-2E26
NORAD 69899
NOAA 17 DEB
NORAD 48165
4.154 14.98 9.2e-08
2026-10-15 06:26:36 FOSSASAT-2E26
NORAD 69899
REPLICATOR 2
NORAD 69927
4.510 0.02 2.2e-07
2026-10-16 08:19:04 YAM-10
NORAD 64580
FOSSASAT-2E26
NORAD 69899
3.848 14.35 1.3e-07
2026-10-16 09:47:45 FOSSASAT-2E26
NORAD 69899
DELTA 1 DEB
NORAD 7892
2.315 7.58 7.3e-07
2026-10-16 09:55:40 YAM-10
NORAD 64580
FOSSASAT-2E26
NORAD 69899
3.042 14.35 2.1e-07
2026-10-16 21:04:23 LEMUR-2-CARROLLEMO
NORAD 68489
FOSSASAT-2E26
NORAD 69899
4.463 7.23 2.0e-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