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FOSSASA-2E23

In orbit NORAD 66788 MWQR-1890-2859-5778-6818

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FOSSASA-2E23
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
488.22 km
Apogee
497.61 km
Inclination
97.4°
Period
94.5 min
Semi-major axis
6871.0 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:37 UTC
Two-line elements (TLE)
1 66788U 25276EC  26284.94342062  .00011387  00000-0  48234-3 0  9993
2 66788 97.4141 357.1743 0006808 80.1740 280.0265 15.23300035 48192
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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 07:15:27 FOSSASA-2E23
NORAD 66788
CAS500-2
NORAD 69013
4.287 15.10 8.5e-08
2026-10-12 17:09:32 TRANSPORTER-15 OBJECT CX
NORAD 66759
FOSSASA-2E23
NORAD 66788
0.821 0.03 6.5e-06
2026-10-13 06:14:38 FOSSASA-2E23
NORAD 66788
COSMOS 2251 DEB
NORAD 34451
4.170 15.20 8.7e-08
2026-10-13 19:11:07 SCS-01 J
NORAD 63990
FOSSASA-2E23
NORAD 66788
3.936 0.27 2.8e-07
2026-10-13 21:54:21 ION SCV-017
NORAD 63230
FOSSASA-2E23
NORAD 66788
1.150 15.09 1.2e-06
2026-10-14 03:03:51 AE5RC
NORAD 66677
FOSSASA-2E23
NORAD 66788
3.923 0.05 2.9e-07
2026-10-14 08:44:46 FOSSASA-2E23
NORAD 66788
SL-24 R/B
NORAD 36606
4.230 15.03 9.5e-08
2026-10-14 12:31:32 FOSSASA-2E23
NORAD 66788
LUCA (RS90S)
NORAD 67287
2.000 0.17 1.1e-06
2026-10-15 06:42:02 FOSSASA-2E23
NORAD 66788
TRANSPORTER-16 OBJECT L
NORAD 68426
0.087 12.69 3.6e-04
2026-10-15 23:59:17 FOSSASA-2E23
NORAD 66788
COSMOS 2607
NORAD 67681
4.306 2.85 2.3e-07
2026-10-16 05:33:32 FOSSASA-2E23
NORAD 66788
AIGLONSAT-1
NORAD 68437
4.278 12.74 1.5e-07
2026-10-16 07:55:28 FOSSASA-2E23
NORAD 66788
AIGLONSAT-1
NORAD 68437
3.681 12.70 2.0e-07
2026-10-17 11:27:41 BALKAN-1
NORAD 62611
FOSSASA-2E23
NORAD 66788
2.540 0.74 6.8e-07
2026-10-17 19:40:53 FOSSASA-2E23
NORAD 66788
GEN1A-2
NORAD 69005
3.533 15.10 1.3e-07
2026-10-17 21:04:46 SPACEMOBILE-003
NORAD 61045
FOSSASA-2E23
NORAD 66788
4.540 12.03 1.4e-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