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: 16 hours ago
TLE from 16 hours ago
0 PERSEUS M1
1 40039U 14033AF 25261.22806426 .00002183 00000-0 20947-3 0 9992
2 40039 97.9325 196.6744 0013414 116.0457 244.2145 14.94103798610002Epoch: 2025-09-18T05:28Z
TLE epoch observation values (Epoch: 2025-09-18T05:28:24.752Z)
Latitude
-0.00002°
Longitude
117.17859°
Altitude
592.27 km
Speed
7.562 km/s
True Right ascension
13h 06m 41s
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
14:41:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.516 km
Perigee altitude
572.843 km
Semi-major axis
6,960.316 km
Eccentricity
0.00134
Inclination
97.9325°
RAAN
196.6744°
Arg. of periapsis
116.0457°
True anomaly
244.07619°
Mean anomaly
244.2145°
Eccentric anomaly
244.14534°
Mean motion
3.73766 °/min
Orbital period
96.32 mins
BSTAR
0.00020947
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-19 07:46:27.339Z | 49.555° ENE | 2025-09-19 07:49:27.339Z | 100.316° ESE | 18.685° | 2025-09-19 07:51:27.339Z | 134.343° SE |
| 5 mins | 2025-09-19 09:22:27.339Z | 336.932° NNW | 2025-09-19 09:24:27.339Z | 293.627° NW | 26.346° | 2025-09-19 09:27:27.339Z | 234.277° WSW |
| 5 mins | 2025-09-19 20:11:27.339Z | 199.015° SSW | 2025-09-19 20:13:27.339Z | 258.963° W | 36.387° | 2025-09-19 20:16:27.339Z | 330.239° NNW |
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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