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: 15 hours ago
TLE from 15 hours ago
0 PERSEUS M1
1 40039U 14033AF 25256.27216607 .00001116 00000-0 10987-3 0 9995
2 40039 97.9315 191.6695 0013047 130.9797 229.2553 14.94083563609264Epoch: 2025-09-13T06:31Z
TLE epoch observation values (Epoch: 2025-09-13T06:31:55.148Z)
Latitude
-0.00006°
Longitude
101.18182°
Altitude
594.196 km
Speed
7.56 km/s
True Right ascension
12h 46m 40s
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
13:52:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.323 km
Perigee altitude
573.161 km
Semi-major axis
6,960.379 km
Eccentricity
0.0013
Inclination
97.9315°
RAAN
191.6695°
Arg. of periapsis
130.9797°
True anomaly
229.14215°
Mean anomaly
229.2553°
Eccentric anomaly
229.19871°
Mean motion
3.73761 °/min
Orbital period
96.32 mins
BSTAR
0.00010987
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-14 08:48:35.851Z | 7.486° NNE | 2025-09-14 08:52:35.851Z | 239.143° WSW | 42.147° | 2025-09-14 08:55:35.851Z | 201.765° SSW |
| 6 mins | 2025-09-14 19:38:35.851Z | 153.415° SSE | 2025-09-14 19:40:35.851Z | 110.77° ESE | 42.186° | 2025-09-14 19:44:35.851Z | 353.214° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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