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: 1 day ago
TLE from 1 day ago
0 MANDRAKE 2 ABLE
1 48907U 21059AE 26187.98923791 .00016663 00000-0 24258-3 0 9993
2 48907 97.7037 19.2949 0003509 274.1422 85.9430 15.55818938280200Epoch: 2026-07-06T23:44Z
TLE epoch observation values (Epoch: 2026-07-06T23:44:30.155Z)
Latitude
-0.00007°
Longitude
98.20295°
Altitude
402.736 km
Speed
7.669 km/s
True Right ascension
01h 17m 10s
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
14:13:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
399.082 km
Perigee altitude
394.327 km
Semi-major axis
6,774.842 km
Eccentricity
0.00035
Inclination
97.7037°
RAAN
19.2949°
Arg. of periapsis
274.1422°
True anomaly
85.98311°
Mean anomaly
85.943°
Eccentric anomaly
85.96306°
Mean motion
3.89219 °/min
Orbital period
92.49 mins
BSTAR
0.00024258
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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 | 2026-07-08 12:56:07.444Z | 177.549° S | 2026-07-08 12:57:07.444Z | 197.764° SSW | 40.874° | 2026-07-08 13:00:07.444Z | 342.988° N |
| 5 mins | 2026-07-09 01:42:07.444Z | 12.997° NNE | 2026-07-09 01:44:07.444Z | 170.586° S | 44.948° | 2026-07-09 01:47:07.444Z | 192.836° 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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