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: 18 hours ago
TLE from 18 hours ago
0 SKYSAT 2
1 40072U 14037D 25320.78444976 .00003336 00000-0 37744-3 0 9992
2 40072 98.3567 263.1291 0004314 241.9957 118.0822 14.87190671614384Epoch: 2025-11-16T18:49Z
TLE epoch observation values (Epoch: 2025-11-16T18:49:36.459Z)
Latitude
0.00006°
Longitude
-75.36709°
Altitude
611.155 km
Speed
7.553 km/s
True Right ascension
17h 32m 30s
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
09:40:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.783 km
Perigee altitude
600.759 km
Semi-major axis
6,981.908 km
Eccentricity
0.00043
Inclination
98.3567°
RAAN
263.1291°
Arg. of periapsis
241.9957°
True anomaly
118.1258°
Mean anomaly
118.0822°
Eccentric anomaly
118.104°
Mean motion
3.72033 °/min
Orbital period
96.77 mins
BSTAR
0.00037744
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Other satellites on launch #37 in the year 2014 (2014-07-08 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-17 19:12:47.350Z | 98.312° ESE | 2025-11-17 19:14:47.350Z | 66.635° ENE | 16.501° | 2025-11-17 19:16:47.350Z | 34.264° NE |
| 6 mins | 2025-11-17 20:47:47.350Z | 200.864° SSW | 2025-11-17 20:50:47.350Z | 278.199° WNW | 32.019° | 2025-11-17 20:53:47.350Z | 328.397° NNW |
| 5 mins | 2025-11-18 08:33:47.350Z | 51.42° ENE | 2025-11-18 08:35:47.350Z | 93.934° ESE | 26.257° | 2025-11-18 08:38:47.350Z | 152.008° SSE |
| 4 mins | 2025-11-18 10:09:47.350Z | 325.872° NNW | 2025-11-18 10:11:47.350Z | 287.084° WNW | 20.715° | 2025-11-18 10:13:47.350Z | 252.255° W |
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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