MANDRAKE 2 ABLE, 48907
Orbit data source: Space-Track
MANDRAKE 2 ABLE, 48907 is an American payload satellite in SSO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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48907 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Astro Digital
Mission
Operational Defense Communications
Bus & Motor
CORVUS-XL, Unknown motor
Mass
23 kg wet, 23 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.3 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 MANDRAKE 2 ABLE
1 48907U 21059AE 25260.99168929 .00014610 00000-0 34096-3 0 9990
2 48907 97.6978 67.7008 0004748 266.7232 93.3471 15.42318749234993Epoch: 2025-09-17T23:48Z
TLE epoch observation values (Epoch: 2025-09-17T23:48:01.954Z)
Latitude
-0.00005°
Longitude
73.53297°
Altitude
442.57 km
Speed
7.646 km/s
True Right ascension
04h 30m 48s
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
19:17:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
439.452 km
Perigee altitude
432.981 km
Semi-major axis
6,814.354 km
Eccentricity
0.00047
Inclination
97.6978°
RAAN
67.7008°
Arg. of periapsis
266.7232°
True anomaly
93.40141°
Mean anomaly
93.3471°
Eccentric anomaly
93.37426°
Mean motion
3.85839 °/min
Orbital period
93.3 mins
BSTAR
0.00034096
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Other satellites on launch #59 in the year 2021 (2021-06-30 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.MANDRAKE 2 ABLE 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 | 2025-09-19 11:45:17.759Z | 212.434° SW | 2025-09-19 11:47:17.759Z | 274.074° WNW | 26.969° | 2025-09-19 11:49:17.759Z | 320.169° NNW |
| 4 mins | 2025-09-20 00:38:17.759Z | 337.022° NNW | 2025-09-20 00:40:17.759Z | 277.317° WNW | 26.647° | 2025-09-20 00:42:17.759Z | 230.987° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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