PERSEUS M2, 40037
Orbit data source: Space-Track
PERSEUS M2, 40037 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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40037 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: 5 hours ago
TLE from 5 hours ago
0 PERSEUS M2
1 40037U 14033AD 26101.28418856 .00002719 00000-0 25190-3 0 9996
2 40037 97.9914 50.4975 0012407 153.3258 206.8603 14.95313547640788Epoch: 2026-04-11T06:49Z
TLE epoch observation values (Epoch: 2026-04-11T06:49:13.891Z)
Latitude
-0°
Longitude
108.68392°
Altitude
592.146 km
Speed
7.56 km/s
True Right ascension
03h 21m 59s
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
18:33:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.055 km
Perigee altitude
569.793 km
Semi-major axis
6,956.561 km
Eccentricity
0.00124
Inclination
97.9914°
RAAN
50.4975°
Arg. of periapsis
153.3258°
True anomaly
206.79615°
Mean anomaly
206.8603°
Eccentric anomaly
206.82822°
Mean motion
3.74069 °/min
Orbital period
96.24 mins
BSTAR
0.0002519
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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 M2 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 | 2026-04-11 19:48:27.485Z | 123.576° SE | 2026-04-11 19:51:27.485Z | 72.821° E | 23.712° | 2026-04-11 19:54:27.485Z | 17.535° NNE |
| 4 mins | 2026-04-11 21:25:27.485Z | 234.951° WSW | 2026-04-11 21:26:27.485Z | 255.403° W | 21.42° | 2026-04-11 21:29:27.485Z | 311.397° NW |
| 5 mins | 2026-04-12 09:06:27.485Z | 38.015° NE | 2026-04-12 09:08:27.485Z | 94.949° ESE | 35.848° | 2026-04-12 09:11:27.485Z | 168.701° S |
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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