PERSEUS M1, 40039
Orbit data source: Space-Track
PERSEUS M1, 40039 is a payload satellite owned by Canopus Sys (CIS) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40039 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
None
Manufacturer
Canopus Sys
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.105 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 PERSEUS M1
1 40039U 14033AF 25327.38364634 .00003047 00000-0 28666-3 0 9998
2 40039 97.9442 263.5562 0009957 259.6922 100.3175 14.94622536619888Epoch: 2025-11-23T09:12Z
TLE epoch observation values (Epoch: 2025-11-23T09:12:27.043Z)
Latitude
-0.00008°
Longitude
62.84478°
Altitude
587.833 km
Speed
7.566 km/s
True Right ascension
17h 34m 13s
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
18:17:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.497 km
Perigee altitude
573.639 km
Semi-major axis
6,958.705 km
Eccentricity
0.001
Inclination
97.9442°
RAAN
263.5562°
Arg. of periapsis
259.6922°
True anomaly
100.42973°
Mean anomaly
100.3175°
Eccentric anomaly
100.37362°
Mean motion
3.73896 °/min
Orbital period
96.28 mins
BSTAR
0.00028666
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.PERSEUS M1 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-24 08:16:28.212Z | 32.63° NE | 2025-11-24 08:19:28.212Z | 85.427° E | 30.737° | 2025-11-24 08:23:28.212Z | 165.742° S |
| 4 mins | 2025-11-24 09:53:28.212Z | 318.446° NNW | 2025-11-24 09:54:28.212Z | 301.549° NW | 16.325° | 2025-11-24 09:57:28.212Z | 253.906° W |
| 5 mins | 2025-11-24 19:06:28.212Z | 108.662° ESE | 2025-11-24 19:08:28.212Z | 69.196° E | 22.432° | 2025-11-24 19:11:28.212Z | 17.747° NNE |
| 5 mins | 2025-11-24 20:41:28.212Z | 219.143° SW | 2025-11-24 20:43:28.212Z | 257.21° W | 23.19° | 2025-11-24 20:46:28.212Z | 314.136° NW |
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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