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: 9 hours ago
TLE from 9 hours ago
0 UMBRA-10
1 60547U 24149CH 26080.51797446 .00026367 00000-0 14040-2 0 9996
2 60547 97.6983 166.4341 0000851 184.6166 175.5058 15.15195882 87446Epoch: 2026-03-21T12:25Z
TLE epoch observation values (Epoch: 2026-03-21T12:25:52.993Z)
Latitude
-0.00001°
Longitude
160.92576°
Altitude
524.045 km
Speed
7.601 km/s
True Right ascension
11h 05m 44s
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
02:34:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
517.956 km
Perigee altitude
516.782 km
Semi-major axis
6,895.506 km
Eccentricity
0.00009
Inclination
97.6983°
RAAN
166.4341°
Arg. of periapsis
184.6166°
True anomaly
175.50656°
Mean anomaly
175.5058°
Eccentric anomaly
175.50618°
Mean motion
3.79048 °/min
Orbital period
94.97 mins
BSTAR
0.001404
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-22 05:59:52.545Z | 189.222° SSW | 2026-03-22 06:02:52.545Z | 288.561° WNW | 36.173° | 2026-03-22 06:05:52.545Z | 336.323° NNW |
| 5 mins | 2026-03-22 19:06:52.545Z | 342.234° N | 2026-03-22 19:08:52.545Z | 296.177° NW | 28.339° | 2026-03-22 19:11:52.545Z | 228.381° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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