SKYSAT 2, 40072
Orbit data source: Space-Track
SKYSAT 2, 40072 is a payload satellite owned by Skybox (US) in SSO that was launched on Tue, 08 Jul 2014 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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40072 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Skybox
Mission
Operational Commercial Imaging
Bus & Motor
SKYSAT, Unknown motor
Mass
82 kg wet, 82 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.800 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SKYSAT 2
1 40072U 14037D 25301.40646250 .00002762 00000-0 31456-3 0 9995
2 40072 98.3530 242.7470 0004779 323.7365 36.3525 14.87065667611502Epoch: 2025-10-28T09:45Z
TLE epoch observation values (Epoch: 2025-10-28T09:45:18.359Z)
Latitude
-0.00005°
Longitude
59.4261°
Altitude
607.438 km
Speed
7.557 km/s
True Right ascension
16h 10m 59s
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
05:28:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
607.499 km
Perigee altitude
600.825 km
Semi-major axis
6,982.299 km
Eccentricity
0.00048
Inclination
98.353°
RAAN
242.747°
Arg. of periapsis
323.7365°
True anomaly
36.38498°
Mean anomaly
36.3525°
Eccentric anomaly
36.36874°
Mean motion
3.72002 °/min
Orbital period
96.77 mins
BSTAR
0.00031456
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Other satellites on launch #37 in the year 2014 (2014-07-08 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.SKYSAT 2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-29 19:48:46.198Z | 136.1° SSE | 2025-10-29 19:50:46.198Z | 93.95° ESE | 34.854° | 2025-10-29 19:54:46.198Z | 1.622° NNE |
| 7 mins | 2025-10-30 09:09:46.198Z | 12.806° NNE | 2025-10-30 09:12:46.198Z | 244.269° WSW | 44.988° | 2025-10-30 09:16:46.198Z | 194.868° SSW |
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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