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, 0.2 m
Radar Cross Section
0.080 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 26303.36335198 .00000538 00000-0 53416-4 0 9998
2 40039 97.9803 249.8398 0010642 201.9739 158.1027 14.96002672670847Epoch: 2026-10-30T08:43Z
TLE epoch observation values (Epoch: 2026-10-30T08:43:13.611Z)
Latitude
0.00005°
Longitude
80.34858°
Altitude
589.176 km
Speed
7.562 km/s
True Right ascension
16h 39m 21s
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
16:08:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.686 km
Perigee altitude
568.885 km
Semi-major axis
6,954.422 km
Eccentricity
0.00106
Inclination
97.9803°
RAAN
249.8398°
Arg. of periapsis
201.9739°
True anomaly
158.14812°
Mean anomaly
158.1027°
Eccentric anomaly
158.12542°
Mean motion
3.74241 °/min
Orbital period
96.19 mins
BSTAR
0.000053416
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-30 21:41:59.373Z | 234.902° WSW | 2026-10-30 21:43:59.373Z | 266.079° W | 15.668° | 2026-10-30 21:45:59.373Z | 297.731° NW |
| 6 mins | 2026-10-31 09:22:59.373Z | 19.493° NNE | 2026-10-31 09:24:59.373Z | 49.478° ENE | 66.55° | 2026-10-31 09:28:59.373Z | 187.544° SSW |
| 6 mins | 2026-10-31 20:10:59.373Z | 134.024° SE | 2026-10-31 20:12:59.373Z | 86.208° E | 43.792° | 2026-10-31 20:16:59.373Z | 1.652° 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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