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: 12 hours ago
TLE from 12 hours ago
0 PERSEUS M1
1 40039U 14033AF 25338.29591635 .00004894 00000-0 45605-3 0 9996
2 40039 97.9447 274.6018 0010759 218.9265 141.1181 14.94689512621512Epoch: 2025-12-04T07:06Z
TLE epoch observation values (Epoch: 2025-12-04T07:06:07.172Z)
Latitude
-0.00005°
Longitude
94.71752°
Altitude
592.212 km
Speed
7.561 km/s
True Right ascension
18h 18m 24s
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
16:32:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.847 km
Perigee altitude
572.873 km
Semi-major axis
6,958.497 km
Eccentricity
0.00108
Inclination
97.9447°
RAAN
274.6018°
Arg. of periapsis
218.9265°
True anomaly
141.19541°
Mean anomaly
141.1181°
Eccentric anomaly
141.15676°
Mean motion
3.73913 °/min
Orbital period
96.28 mins
BSTAR
0.00045605
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-04 20:04:33.817Z | 175.253° S | 2025-12-04 20:07:33.817Z | 213.597° SW | 41.688° | 2025-12-04 20:11:33.817Z | 341.471° N |
| 4 mins | 2025-12-05 07:48:33.817Z | 68.741° E | 2025-12-05 07:49:33.817Z | 85.569° E | 15.893° | 2025-12-05 07:52:33.817Z | 133.255° SE |
| 5 mins | 2025-12-05 09:23:33.817Z | 337.77° N | 2025-12-05 09:25:33.817Z | 285.059° WNW | 30.302° | 2025-12-05 09:28:33.817Z | 226.439° 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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