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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 (2 years 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: 16 hours ago

TLE from 16 hours ago
0 DEIMOS
1 60526U 24149BL  26080.19136423  .00022918  00000-0  55830-3 0  9990
2 60526  97.3804 165.2410 0004907 231.1939 128.8869 15.40914093 88889
Epoch: 2026-03-21T04:35Z
TLE epoch observation values (Epoch: 2026-03-21T04:35:33.869Z)
Latitude
-0.0001°
Longitude
-82.36573°
Altitude
448.632 km
Speed
7.642 km/s
True Right ascension
11h 00m 57s
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
01:03:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.693 km
Perigee altitude
437.001 km
Semi-major axis
6,818.484 km
Eccentricity
0.00049
Inclination
97.3804°
RAAN
165.241°
Arg. of periapsis
231.1939°
True anomaly
128.93065°
Mean anomaly
128.8869°
Eccentric anomaly
128.90878°
Mean motion
3.85488 °/min
Orbital period
93.39 mins
BSTAR
0.0005583
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