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DEIMOS, 60526

Orbit data source: Space-Track

DEIMOS, 60526 is an American payload satellite in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
60526, 2024-149BL
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Endurosat
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
2024-08-16 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.025 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 DEIMOS
1 60526U 24149BL  25353.18573199  .00014259  00000-0  39647-3 0  9993
2 60526  97.3954  72.5038 0005681 204.7476 155.3496 15.36944946 74738
Epoch: 2025-12-19T04:27Z
TLE epoch observation values (Epoch: 2025-12-19T04:27:27.243Z)
Latitude
-0.00011°
Longitude
-82.39021°
Altitude
461.793 km
Speed
7.634 km/s
True Right ascension
04h 50m 00s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
17:29:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.973 km
Perigee altitude
448.212 km
Semi-major axis
6,830.229 km
Eccentricity
0.00057
Inclination
97.3954°
RAAN
72.5038°
Arg. of periapsis
204.7476°
True anomaly
155.37673°
Mean anomaly
155.3496°
Eccentric anomaly
155.36317°
Mean motion
3.84495 °/min
Orbital period
93.63 mins
BSTAR
0.00039647
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Documentation

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