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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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: 8 hours ago
TLE from 8 hours ago
0 PERSEUS M1
1 40039U 14033AF 26078.77874463 .00002111 00000-0 19698-3 0 9997
2 40039 97.9566 21.5080 0010375 229.4892 130.5425 14.95297569637270Epoch: 2026-03-19T18:41Z
TLE epoch observation values (Epoch: 2026-03-19T18:41:23.536Z)
Latitude
0.00001°
Longitude
-76.16334°
Altitude
589.189 km
Speed
7.563 km/s
True Right ascension
01h 26m 01s
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
08:00:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.69 km
Perigee altitude
571.255 km
Semi-major axis
6,956.609 km
Eccentricity
0.00104
Inclination
97.9566°
RAAN
21.508°
Arg. of periapsis
229.4892°
True anomaly
130.63277°
Mean anomaly
130.5425°
Eccentric anomaly
130.58764°
Mean motion
3.74065 °/min
Orbital period
96.24 mins
BSTAR
0.00019698
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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 | 2026-03-20 08:07:26.784Z | 49.747° ENE | 2026-03-20 08:10:26.784Z | 101.786° ESE | 19.295° | 2026-03-20 08:12:26.784Z | 135.879° SSE |
| 5 mins | 2026-03-20 09:43:26.784Z | 334.234° NNW | 2026-03-20 09:45:26.784Z | 289.546° WNW | 25.937° | 2026-03-20 09:48:26.784Z | 233.933° WSW |
| 6 mins | 2026-03-20 20:31:26.784Z | 197.001° SSW | 2026-03-20 20:33:26.784Z | 246.67° WSW | 35.679° | 2026-03-20 20:37:26.784Z | 333.857° 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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