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: 1 day ago
TLE from 1 day ago
0 PERSEUS M1
1 40039U 14033AF 25312.38680606 .00004018 00000-0 37727-3 0 9999
2 40039 97.9417 248.3822 0010624 317.5093 42.5304 14.94504638617641Epoch: 2025-11-08T09:17Z
TLE epoch observation values (Epoch: 2025-11-08T09:17:00.043Z)
Latitude
0.00002°
Longitude
61.31486°
Altitude
581.502 km
Speed
7.573 km/s
True Right ascension
16h 33m 31s
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
16:04:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.327 km
Perigee altitude
573.541 km
Semi-major axis
6,959.071 km
Eccentricity
0.00106
Inclination
97.9417°
RAAN
248.3822°
Arg. of periapsis
317.5093°
True anomaly
42.61278°
Mean anomaly
42.5304°
Eccentric anomaly
42.57158°
Mean motion
3.73866 °/min
Orbital period
96.29 mins
BSTAR
0.00037727
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-09 20:45:24.489Z | 215.555° SW | 2025-11-09 20:48:24.489Z | 264.975° W | 20.278° | 2025-11-09 20:51:24.489Z | 314.398° NW |
| 6 mins | 2025-11-10 08:28:24.489Z | 34.202° NE | 2025-11-10 08:30:24.489Z | 92.884° ESE | 38.385° | 2025-11-10 08:34:24.489Z | 177.074° S |
| 5 mins | 2025-11-10 19:17:24.489Z | 113.973° SE | 2025-11-10 19:19:24.489Z | 62.081° ENE | 27.999° | 2025-11-10 19:22:24.489Z | 10.027° NNE |
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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