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 (25 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: 9 hours ago

TLE from 9 hours ago
0 MAROC TUBSAT
1 27004U 01056D   26214.51526353 -.00000037  00000-0  10673-4 0  9992
2 27004  99.8113  32.2548 0020179  26.5128  42.9404 13.70264195232539
Epoch: 2026-08-02T12:21Z
TLE epoch observation values (Epoch: 2026-08-02T12:21:58.768Z)
Latitude
67.54677°
Longitude
-128.95246°
Altitude
999.343 km
Speed
7.364 km/s
True Right ascension
00h 30m 36s
True Declination
67° 25' 45"
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
10:49:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,010.783 km
Perigee altitude
981.023 km
Semi-major axis
7,374.04 km
Eccentricity
0.00202
Inclination
99.8113°
RAAN
32.2548°
Arg. of periapsis
26.5128°
True anomaly
43.09822°
Mean anomaly
42.9404°
Eccentric anomaly
43.01928°
Mean motion
3.42756 °/min
Orbital period
105.03 mins
BSTAR
0.000010673
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
|