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SPARTAN, 48964

Orbit data source: Space-Track

SPARTAN, 48964 is a payload satellite owned by Endurosat (BG) 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.

Not visible in the next 10 days
Identifier
48964, 2021-059CP
Orbit
SSO
Country
Flag of BGBG / BGR
Related business
Manufacturer
Endurosat
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 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 + 2 Pan, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 SPARTAN
1 48964U 21059CP  26250.55999093  .00322186  48276-4  51019-3 0  9994
2 48964  97.6652 101.6244 0001272 247.6088 112.5057 16.03831855291017
Epoch: 2026-09-07T13:26Z
TLE epoch observation values (Epoch: 2026-09-07T13:26:23.216Z)
Latitude
0.00001°
Longitude
-86.61134°
Altitude
267.337 km
Speed
7.747 km/s
True Right ascension
06h 46m 29s
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
05:59:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
261.53 km
Perigee altitude
259.841 km
Semi-major axis
6,638.822 km
Eccentricity
0.00013
Inclination
97.6652°
RAAN
101.6244°
Arg. of periapsis
247.6088°
True anomaly
112.51917°
Mean anomaly
112.5057°
Eccentric anomaly
112.51243°
Mean motion
4.01242 °/min
Orbital period
89.72 mins
BSTAR
0.00051019
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Computing Atmospheric mass density...

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