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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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 DEIMOS
1 60526U 24149BL 25297.73620777 .00019996 00000-0 59991-3 0 9993
2 60526 97.3996 16.8199 0007428 60.8820 299.3166 15.34470652 66222Epoch: 2025-10-24T17:40Z
TLE epoch observation values (Epoch: 2025-10-24T17:40:08.351Z)
Latitude
0.00001°
Longitude
78.40827°
Altitude
463.118 km
Speed
7.636 km/s
True Right ascension
01h 07m 16s
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
20:07:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.518 km
Perigee altitude
454.361 km
Semi-major axis
6,837.577 km
Eccentricity
0.00074
Inclination
97.3996°
RAAN
16.8199°
Arg. of periapsis
60.882°
True anomaly
299.24235°
Mean anomaly
299.3166°
Eccentric anomaly
299.27948°
Mean motion
3.83875 °/min
Orbital period
93.78 mins
BSTAR
0.00059991
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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 | 2025-10-25 04:46:03.640Z | 121.977° SE | 2025-10-25 04:48:03.640Z | 83.281° E | 21.335° | 2025-10-25 04:51:03.640Z | 18.366° NNE |
| 4 mins | 2025-10-25 17:44:03.640Z | 59.545° ENE | 2025-10-25 17:45:03.640Z | 87.797° E | 25.323° | 2025-10-25 17:48:03.640Z | 156.333° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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