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 25306.38567405 .00002481 00000-0 28310-3 0 9994
2 40072 98.3538 247.9832 0004478 304.0618 56.0171 14.87091582612241Epoch: 2025-11-02T09:15Z
TLE epoch observation values (Epoch: 2025-11-02T09:15:22.237Z)
Latitude
-0.00005°
Longitude
67.2384°
Altitude
608.298 km
Speed
7.556 km/s
True Right ascension
16h 31m 55s
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
08:09:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
607.207 km
Perigee altitude
600.954 km
Semi-major axis
6,982.218 km
Eccentricity
0.00045
Inclination
98.3538°
RAAN
247.9832°
Arg. of periapsis
304.0618°
True anomaly
56.05966°
Mean anomaly
56.0171°
Eccentric anomaly
56.03838°
Mean motion
3.72009 °/min
Orbital period
96.77 mins
BSTAR
0.0002831
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-03 19:18:39.903Z | 116.901° SE | 2025-11-03 19:21:39.903Z | 70.832° E | 20.439° | 2025-11-03 19:24:39.903Z | 20.824° NNE |
| 5 mins | 2025-11-03 20:55:39.903Z | 221.131° SW | 2025-11-03 20:57:39.903Z | 268.593° W | 26.645° | 2025-11-03 21:00:39.903Z | 320.927° NNW |
| 6 mins | 2025-11-04 08:40:39.903Z | 40.858° NE | 2025-11-04 08:42:39.903Z | 83.607° E | 31.727° | 2025-11-04 08:46:39.903Z | 166.622° S |
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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