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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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, 1.5 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 MANDRAKE 2 ABLE
1 48907U 21059AE 26140.49223399 .00015822 00000-0 24806-3 0 9990
2 48907 97.7044 328.1899 0006273 95.5013 264.6956 15.53776475272821Epoch: 2026-05-20T11:48Z
TLE epoch observation values (Epoch: 2026-05-20T11:48:49.016Z)
Latitude
0.00004°
Longitude
-87.16535°
Altitude
409.235 km
Speed
7.665 km/s
True Right ascension
21h 52m 45s
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
15:53:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
406.899 km
Perigee altitude
398.392 km
Semi-major axis
6,780.783 km
Eccentricity
0.00063
Inclination
97.7044°
RAAN
328.1899°
Arg. of periapsis
95.5013°
True anomaly
264.62403°
Mean anomaly
264.6956°
Eccentric anomaly
264.65981°
Mean motion
3.88708 °/min
Orbital period
92.61 mins
BSTAR
0.00024806
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-21 12:39:57.850Z | 175.259° S | 2026-05-21 12:42:57.850Z | 270.104° WNW | 42.41° | 2026-05-21 12:44:57.850Z | 338.532° N |
| 4 mins | 2026-05-22 01:28:57.850Z | 6.756° NNE | 2026-05-22 01:29:57.850Z | 351.974° N | 41.83° | 2026-05-22 01:32:57.850Z | 197.124° SSW |
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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