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: 2 days ago
TLE from 2 days ago
0 PERSEUS M1
1 40039U 14033AF 26171.38128338 .00001465 00000-0 13720-3 0 9992
2 40039 97.9641 115.5653 0010078 289.2139 70.7991 14.95639538651110Epoch: 2026-06-20T09:09Z
TLE epoch observation values (Epoch: 2026-06-20T09:09:02.884Z)
Latitude
0.00006°
Longitude
69.70655°
Altitude
581.129 km
Speed
7.571 km/s
True Right ascension
07h 42m 15s
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
21:42:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.421 km
Perigee altitude
570.401 km
Semi-major axis
6,955.548 km
Eccentricity
0.00101
Inclination
97.9641°
RAAN
115.5653°
Arg. of periapsis
289.2139°
True anomaly
70.90821°
Mean anomaly
70.7991°
Eccentric anomaly
70.85365°
Mean motion
3.7415 °/min
Orbital period
96.22 mins
BSTAR
0.0001372
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 20:41:28.336Z | 192.497° SSW | 2026-06-22 20:44:28.336Z | 276.778° WNW | 35.94° | 2026-06-22 20:47:28.336Z | 332.435° NNW |
| 5 mins | 2026-06-23 08:23:28.336Z | 52.655° ENE | 2026-06-23 08:25:28.336Z | 88.879° E | 21.331° | 2026-06-23 08:28:28.336Z | 143.255° SSE |
| 4 mins | 2026-06-23 09:59:28.336Z | 325.011° NNW | 2026-06-23 10:01:28.336Z | 278.73° WNW | 23.572° | 2026-06-23 10:03:28.336Z | 242.727° 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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