Showing default

MAROC TUBSAT, 27004

Orbit data source: Space-Track

MAROC TUBSAT, 27004 is a payload satellite owned by CRTS (DE) in SSO that was launched on Mon, 10 Dec 2001 UTC via a ZENIT-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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
27004, 2001-056D
Orbit
SSO
Country
Flag of DEDE / GER
Related business
Manufacturer
TUB
Mission
Operational Civil Imaging
Bus & Motor
TUBSAT, Unknown motor
Mass
45 kg wet, 45 kg dry
Launch date (UTC)
2001-12-10 (24 years ago)
Launch vehicle
ZENIT-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.200 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 MAROC TUBSAT
1 27004U 01056D   25303.08171248 -.00000010  00000-0  41819-4 0  9998
2 27004  99.7912 110.7643 0020003  14.6014  95.6779 13.70249899194677
Epoch: 2025-10-30T01:57Z
TLE epoch observation values (Epoch: 2025-10-30T01:57:39.958Z)
Latitude
67.44915°
Longitude
-112.87728°
Altitude
1,011.752 km
Speed
7.351 km/s
True Right ascension
21h 00m 44s
True Declination
67° 19' 53"
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
21:04:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,010.703 km
Perigee altitude
981.203 km
Semi-major axis
7,374.09 km
Eccentricity
0.002
Inclination
99.7912°
RAAN
110.7643°
Arg. of periapsis
14.6014°
True anomaly
95.90594°
Mean anomaly
95.6779°
Eccentric anomaly
95.79192°
Mean motion
3.42752 °/min
Orbital period
105.03 mins
BSTAR
0.000041819
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
|