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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60526 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Endurosat
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 DEIMOS
1 60526U 24149BL 26175.21308061 .00016725 00000-0 36308-3 0 9995
2 60526 97.3780 261.4583 0004333 248.1283 111.9505 15.44439271103539Epoch: 2026-06-24T05:06Z
TLE epoch observation values (Epoch: 2026-06-24T05:06:50.164Z)
Latitude
-0.00003°
Longitude
-87.62424°
Altitude
437.255 km
Speed
7.649 km/s
True Right ascension
17h 25m 49s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:56:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
432.908 km
Perigee altitude
427.008 km
Semi-major axis
6,808.095 km
Eccentricity
0.00043
Inclination
97.378°
RAAN
261.4583°
Arg. of periapsis
248.1283°
True anomaly
111.99654°
Mean anomaly
111.9505°
Eccentric anomaly
111.97352°
Mean motion
3.86371 °/min
Orbital period
93.17 mins
BSTAR
0.00036308
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DEIMOS Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-24 18:07:12.581Z | 39.062° NE | 2026-06-24 18:09:12.581Z | 80.346° E | 24.76° | 2026-06-24 18:12:12.581Z | 156.13° SSE |
| 4 mins | 2026-06-25 06:08:12.581Z | 197.868° SSW | 2026-06-25 06:10:12.581Z | 282.891° WNW | 34.939° | 2026-06-25 06:12:12.581Z | 330.747° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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