UMBRA-09, 60541
Orbit data source: Space-Track
UMBRA-09, 60541 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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60541 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: 10 hours ago
TLE from 10 hours ago
0 UMBRA-09
1 60541U 24149CB 26002.17970667 .00030412 00000-0 17705-2 0 9991
2 60541 97.7100 87.2152 0001491 208.1860 151.9290 15.11970102 75586Epoch: 2026-01-02T04:18Z
TLE epoch observation values (Epoch: 2026-01-02T04:18:46.656Z)
Latitude
0.00005°
Longitude
-79.30284°
Altitude
534.172 km
Speed
7.595 km/s
True Right ascension
05h 48m 51s
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
14:34:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.212 km
Perigee altitude
526.153 km
Semi-major axis
6,905.319 km
Eccentricity
0.00015
Inclination
97.71°
RAAN
87.2152°
Arg. of periapsis
208.186°
True anomaly
151.93704°
Mean anomaly
151.929°
Eccentric anomaly
151.93302°
Mean motion
3.7824 °/min
Orbital period
95.18 mins
BSTAR
0.0017705
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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-09 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 | 2026-01-02 17:36:00.146Z | 49.201° ENE | 2026-01-02 17:39:00.146Z | 106.523° ESE | 19.332° | 2026-01-02 17:41:00.146Z | 140.951° SSE |
| 4 mins | 2026-01-02 19:11:00.146Z | 329.13° NNW | 2026-01-02 19:13:00.146Z | 283.863° WNW | 22.443° | 2026-01-02 19:15:00.146Z | 244.291° WSW |
| 5 mins | 2026-01-03 05:52:00.146Z | 193.273° SSW | 2026-01-03 05:54:00.146Z | 258.97° W | 38.195° | 2026-01-03 05:57:00.146Z | 334.044° 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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