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: 18 hours ago
TLE from 18 hours ago
0 UMBRA-10
1 60547U 24149CH 25289.46185742 .00017663 00000-0 11343-2 0 9992
2 60547 97.7161 8.9679 0001878 106.7383 253.4051 15.08513189 63860Epoch: 2025-10-16T11:05Z
TLE epoch observation values (Epoch: 2025-10-16T11:05:04.481Z)
Latitude
-0.00002°
Longitude
177.47799°
Altitude
544.18 km
Speed
7.59 km/s
True Right ascension
00h 35m 52s
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
23:18:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.036 km
Perigee altitude
536.438 km
Semi-major axis
6,915.874 km
Eccentricity
0.00019
Inclination
97.7161°
RAAN
8.9679°
Arg. of periapsis
106.7383°
True anomaly
253.38448°
Mean anomaly
253.4051°
Eccentric anomaly
253.39479°
Mean motion
3.77374 °/min
Orbital period
95.4 mins
BSTAR
0.0011343
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-17 04:44:26.617Z | 121.689° SE | 2025-10-17 04:47:26.617Z | 59.404° ENE | 23.632° | 2025-10-17 04:49:26.617Z | 21.099° NNE |
| 5 mins | 2025-10-17 17:55:26.617Z | 44.402° NE | 2025-10-17 17:57:26.617Z | 113.114° SE | 33.728° | 2025-10-17 18:00:26.617Z | 169.601° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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