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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Edit Public Description
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: 21 hours ago
TLE from 21 hours ago
0 UMBRA-10
1 60547U 24149CH 25338.51134294 .00042651 00000-0 25627-2 0 9994
2 60547 97.7138 58.3178 0000493 266.4192 93.6981 15.10741637 71264Epoch: 2025-12-04T12:16Z
TLE epoch observation values (Epoch: 2025-12-04T12:16:20.030Z)
Latitude
0.00002°
Longitude
160.6676°
Altitude
537.028 km
Speed
7.594 km/s
True Right ascension
03h 53m 16s
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
07:18:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.269 km
Perigee altitude
530.588 km
Semi-major axis
6,909.066 km
Eccentricity
0.00005
Inclination
97.7138°
RAAN
58.3178°
Arg. of periapsis
266.4192°
True anomaly
93.70374°
Mean anomaly
93.6981°
Eccentric anomaly
93.70092°
Mean motion
3.77932 °/min
Orbital period
95.26 mins
BSTAR
0.0025627
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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 | 2025-12-05 17:28:25.772Z | 57.525° ENE | 2025-12-05 17:30:25.772Z | 93.723° ESE | 17.481° | 2025-12-05 17:32:25.772Z | 130.274° SE |
| 4 mins | 2025-12-05 19:03:25.772Z | 325.81° NNW | 2025-12-05 19:04:25.772Z | 301.694° NW | 24.962° | 2025-12-05 19:07:25.772Z | 235.93° WSW |
| 5 mins | 2025-12-06 05:44:25.772Z | 185.533° SSW | 2025-12-06 05:46:25.772Z | 248.529° W | 41.016° | 2025-12-06 05:49:25.772Z | 337.205° 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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