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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: 5 hours ago

TLE from 5 hours ago
0 DEIMOS
1 60526U 24149BL  26035.16170587  .00021354  00000-0  55322-3 0  9995
2 60526  97.3873 119.8039 0006713  53.3319 306.8543 15.39037661 81953
Epoch: 2026-02-04T03:52Z
TLE epoch observation values (Epoch: 2026-02-04T03:52:51.387Z)
Latitude
0.00003°
Longitude
-72.74247°
Altitude
449.323 km
Speed
7.644 km/s
True Right ascension
07h 59m 12s
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
10:44:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.474 km
Perigee altitude
441.312 km
Semi-major axis
6,824.03 km
Eccentricity
0.00067
Inclination
97.3873°
RAAN
119.8039°
Arg. of periapsis
53.3319°
True anomaly
306.79272°
Mean anomaly
306.8543°
Eccentric anomaly
306.82351°
Mean motion
3.85019 °/min
Orbital period
93.5 mins
BSTAR
0.00055322
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