UMBRA-10, 60547
Orbit data source: Space-Track
UMBRA-10, 60547 is a payload satellite owned by Umbra Labs (US) in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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60547 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Umbra Labs
Mission
Operational Commercial Radar Imaging
Bus & Motor
ESPASAT?, Unknown motor
Mass
84 kg wet, 79 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Dish, 2.0 m
Radar Cross Section
6.513 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 UMBRA-10
1 60547U 24149CH 26265.00916734 .00011775 00000-0 53869-3 0 9998
2 60547 97.6945 354.0817 0000966 55.0928 305.0397 15.20688345115435Epoch: 2026-09-22T00:13Z
TLE epoch observation values (Epoch: 2026-09-22T00:13:12.058Z)
Latitude
-0.00004°
Longitude
-10.09934°
Altitude
506.464 km
Speed
7.611 km/s
True Right ascension
23h 36m 19s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
04:32:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.405 km
Perigee altitude
500.076 km
Semi-major axis
6,878.878 km
Eccentricity
0.0001
Inclination
97.6945°
RAAN
354.0817°
Arg. of periapsis
55.0928°
True anomaly
305.03064°
Mean anomaly
305.0397°
Eccentric anomaly
305.03517°
Mean motion
3.80423 °/min
Orbital period
94.63 mins
BSTAR
0.00053869
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.UMBRA-10 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-22 18:10:33.557Z | 53.601° ENE | 2026-09-22 18:12:33.557Z | 94.282° ESE | 21.816° | 2026-09-22 18:14:33.557Z | 136.009° SSE |
| 4 mins | 2026-09-22 19:44:33.557Z | 327.918° NNW | 2026-09-22 19:46:33.557Z | 284.07° WNW | 22.026° | 2026-09-22 19:48:33.557Z | 245.743° WSW |
| 6 mins | 2026-09-23 06:20:33.557Z | 182.541° SSW | 2026-09-23 06:23:33.557Z | 236.209° WSW | 50.812° | 2026-09-23 06:26:33.557Z | 333.389° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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