Showing default

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.

Loading next visibility...
Identifier
40037, 2014-033AD
Orbit
SSO
Country
Flag of CISCIS
Related 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)
2014-06-19 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.105 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 PERSEUS M2
1 40037U 14033AD  26079.13383840  .00001548  00000-0  14632-3 0  9996
2 40037  97.9875  27.9285 0010602 230.6558 129.3723 14.95200249637472
Epoch: 2026-03-20T03:12Z
TLE epoch observation values (Epoch: 2026-03-20T03:12:43.637Z)
Latitude
-0.00005°
Longitude
162.07341°
Altitude
589.477 km
Speed
7.563 km/s
True Right ascension
01h 51m 42s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:59:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.152 km
Perigee altitude
571.4 km
Semi-major axis
6,956.913 km
Eccentricity
0.00106
Inclination
97.9875°
RAAN
27.9285°
Arg. of periapsis
230.6558°
True anomaly
129.46614°
Mean anomaly
129.3723°
Eccentric anomaly
129.41923°
Mean motion
3.7404 °/min
Orbital period
96.25 mins
BSTAR
0.00014632
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|