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Umbra 10

In orbit NORAD 60547 UEGZ-5587-9074-5300-5132

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
Umbra 10
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
2024-08-16 18:56:00
Separation time
2024-08-16 21:30:22
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
499.09 km
Apogee
499.44 km
Inclination
97.7°
Period
94.7 min
Semi-major axis
6877.4 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:19 UTC
Two-line elements (TLE)
1 60547U 24149CH  26282.97008791  .00017508  00000-0  78751-3 0  9995
2 60547 97.6950 12.4204 0000256 162.5698 197.5546 15.21177171118160
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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 03:53:08 UMBRA-10
NORAD 60547
BSLT-3
NORAD 69009
4.207 14.99 9.3e-08
2026-10-11 05:27:50 UMBRA-10
NORAD 60547
BSLT-3
NORAD 69009
1.856 14.99 4.8e-07
2026-10-11 11:59:18 UMBRA-10
NORAD 60547
TIANYI C
NORAD 64050
1.927 2.69 1.2e-06
2026-10-11 14:21:19 UMBRA-10
NORAD 60547
FOSSASA-2E23
NORAD 66788
4.847 2.26 1.9e-07
2026-10-11 22:30:43 YAOGAN-39 01C
NORAD 57731
UMBRA-10
NORAD 60547
4.703 13.08 1.2e-07
2026-10-11 23:51:35 UMBRA-10
NORAD 60547
TOMORROW-S11
NORAD 67399
1.013 10.79 3.2e-06
2026-10-12 12:26:28 VSP RF B1
NORAD 59137
UMBRA-10
NORAD 60547
4.122 6.20 2.4e-07
2026-10-12 19:13:23 UMBRA-10
NORAD 60547
SEMI-1N
NORAD 66297
4.743 14.39 8.9e-08
2026-10-12 23:29:44 UMBRA-10
NORAD 60547
OBJECT E
NORAD 67750
4.710 4.94 1.9e-07
2026-10-13 14:20:19 STARLINK-5293
NORAD 55295
UMBRA-10
NORAD 60547
4.709 14.97 2.3e-06
2026-10-13 19:51:27 UMBRA-10
NORAD 60547
TOMORROW-S6
NORAD 63225
3.045 14.88 1.8e-07
2026-10-13 23:58:33 UMBRA-10
NORAD 60547
NUSAT-51 (YVONNE BRILL)
NORAD 66740
3.960 2.33 2.8e-07
2026-10-14 01:33:16 UMBRA-10
NORAD 60547
NUSAT-51 (YVONNE BRILL)
NORAD 66740
0.795 2.33 6.9e-06
2026-10-14 02:20:38 UMBRA-10
NORAD 60547
NUSAT-51 (YVONNE BRILL)
NORAD 66740
3.497 2.32 3.6e-07
2026-10-14 03:07:59 UMBRA-10
NORAD 60547
NUSAT-51 (YVONNE BRILL)
NORAD 66740
2.657 2.33 6.2e-07
2026-10-14 03:55:20 UMBRA-10
NORAD 60547
NUSAT-51 (YVONNE BRILL)
NORAD 66740
1.195 2.32 3.1e-06
2026-10-14 05:30:03 UMBRA-10
NORAD 60547
NUSAT-51 (YVONNE BRILL)
NORAD 66740
3.379 2.32 3.8e-07
2026-10-14 12:13:56 UMBRA-10
NORAD 60547
TOMORROW-S9
NORAD 66309
4.274 14.44 1.1e-07
2026-10-15 10:40:22 UMBRA-10
NORAD 60547
NOAA 17 DEB
NORAD 48713
3.218 8.91 3.6e-07
2026-10-15 17:01:04 UMBRA-10
NORAD 60547
OBJECT AE
NORAD 67276
3.278 2.23 4.1e-07
2026-10-16 19:57:40 BISONSAT
NORAD 40974
UMBRA-10
NORAD 60547
2.959 13.22 2.9e-07
2026-10-16 20:19:34 UMBRA-10
NORAD 60547
HULIANWANG JISHU SHIYAN 9C
NORAD 68833
2.137 14.74 3.9e-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