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: 9 hours ago
TLE from 9 hours ago
0 PERSEUS M1
1 40039U 14033AF 25308.36957869 .00003179 00000-0 29989-3 0 9998
2 40039 97.9401 244.3187 0011003 331.3267 28.7347 14.94469483617048Epoch: 2025-11-04T08:52Z
TLE epoch observation values (Epoch: 2025-11-04T08:52:11.598Z)
Latitude
0.00001°
Longitude
67.41279°
Altitude
580.343 km
Speed
7.574 km/s
True Right ascension
16h 17m 16s
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
13:29:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.7 km
Perigee altitude
573.386 km
Semi-major axis
6,959.18 km
Eccentricity
0.0011
Inclination
97.9401°
RAAN
244.3187°
Arg. of periapsis
331.3267°
True anomaly
28.79539°
Mean anomaly
28.7347°
Eccentric anomaly
28.76504°
Mean motion
3.73857 °/min
Orbital period
96.29 mins
BSTAR
0.00029989
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-04 20:15:20.691Z | 195.531° SSW | 2025-11-04 20:17:20.691Z | 245.469° WSW | 36.187° | 2025-11-04 20:21:20.691Z | 334.535° NNW |
| 4 mins | 2025-11-05 07:58:20.691Z | 65.335° ENE | 2025-11-05 07:59:20.691Z | 85.499° E | 21.503° | 2025-11-05 08:02:20.691Z | 141.795° SSE |
| 5 mins | 2025-11-05 09:33:20.691Z | 328.403° NNW | 2025-11-05 09:35:20.691Z | 284.327° WNW | 23.868° | 2025-11-05 09:38:20.691Z | 235.43° WSW |
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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