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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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Identifier
48907, 2021-059AE
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Astro Digital
Mission
Operational Defense Communications
Bus & Motor
CORVUS-XL, Unknown motor
Mass
23 kg wet, 23 kg dry
Launch date (UTC)
2021-06-30 (5 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 MANDRAKE 2 ABLE
1 48907U 21059AE  26311.35359130  .00035939  00000-0  42963-3 0  9993
2 48907  97.6909 152.6542 0004279 161.6725 198.4687 15.60921047299418
Epoch: 2026-11-07T08:29Z
TLE epoch observation values (Epoch: 2026-11-07T08:29:10.288Z)
Latitude
0.00005°
Longitude
-21.19873°
Altitude
390.878 km
Speed
7.674 km/s
True Right ascension
10h 10m 37s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:47:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
384.812 km
Perigee altitude
379.027 km
Semi-major axis
6,760.056 km
Eccentricity
0.00043
Inclination
97.6909°
RAAN
152.6542°
Arg. of periapsis
161.6725°
True anomaly
198.45317°
Mean anomaly
198.4687°
Eccentric anomaly
198.46094°
Mean motion
3.90497 °/min
Orbital period
92.19 mins
BSTAR
0.00042963
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