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UM5Sat-EOsat

In orbit NORAD 60555 YDQM-1508-8291-7641-4635

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

1

Observations all time

Mission information
Spacecraft name
UM5Sat-EOsat
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
550.15 km
Apogee
564.68 km
Inclination
97.7°
Period
95.9 min
Semi-major axis
6935.5 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:57 UTC
Two-line elements (TLE)
1 60555U 24149CR  26283.50183530  .00003510  00000-0  27137-3 0  9999
2 60555 97.6674 0.9336 0010507 111.2136 249.0212 15.02105771117526
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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 05:19:05 UM5-EOSAT
NORAD 60555
SPOT 1
NORAD 16613
0.372 13.96 3.2e-04
2026-10-11 21:19:36 UM5-EOSAT
NORAD 60555
STARLINK-35717
NORAD 66839
3.361 14.45 5.1e-06
2026-10-12 03:44:56 STARLINK-6058
NORAD 56797
UM5-EOSAT
NORAD 60555
3.197 14.74 5.2e-06
2026-10-12 17:52:03 SMDC ONE 2.4
NORAD 39469
UM5-EOSAT
NORAD 60555
3.010 9.79 3.9e-07
2026-10-13 02:04:36 STARLINK-5854
NORAD 55923
UM5-EOSAT
NORAD 60555
3.380 12.68 7.2e-06
2026-10-13 12:50:04 UM5-EOSAT
NORAD 60555
MINOTAUR 1 R/B
NORAD 48849
4.597 5.63 2.0e-07
2026-10-14 19:37:39 UM5-EOSAT
NORAD 60555
VELOX-PII
NORAD 39438
3.680 13.35 1.8e-07
2026-10-14 19:38:39 STARLINK-5863
NORAD 55922
UM5-EOSAT
NORAD 60555
2.749 12.26 1.1e-05
2026-10-14 21:15:13 UM5-EOSAT
NORAD 60555
STARLINK-35997
NORAD 66843
4.582 14.03 3.1e-06
2026-10-14 23:25:02 OBJECT D
NORAD 51949
UM5-EOSAT
NORAD 60555
2.234 14.16 4.2e-07
2026-10-15 03:40:18 UM5-EOSAT
NORAD 60555
NOAA 16 DEB
NORAD 42427
3.507 14.35 1.6e-07
2026-10-15 10:42:01 UM5-EOSAT
NORAD 60555
CZ-4B DEB
NORAD 26127
4.627 12.07 1.4e-07
2026-10-15 15:10:57 YAOGAN-30 07A
NORAD 45460
UM5-EOSAT
NORAD 60555
3.670 13.85 1.7e-07
2026-10-15 21:41:34 YAOGAN-30 03C
NORAD 43030
UM5-EOSAT
NORAD 60555
3.596 12.34 2.2e-07
2026-10-16 21:02:13 STARLINK-5637
NORAD 55432
UM5-EOSAT
NORAD 60555
2.291 11.79 1.7e-05

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