Showing default

HRC MONOBLOCK CAMERA, 66052

Orbit data source: Space-Track

HRC MONOBLOCK CAMERA, 66052 is a payload satellite owned by UrtheCast (CIS) in LEO that was delivered to the ISS. 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
66052, 1998-067XR
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Wet unknown, 82 kg dry
Launch date (UTC)
1998-11-20 (28 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.6 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 HRC MONOBLOCK CAMERA
1 66052U 98067XR  26178.41867543  .00082704  00000-0  53153-3 0  9992
2 66052  51.6213 226.5608 0002667 351.1614   8.9338 15.75493112 39618
Epoch: 2026-06-27T10:02Z
TLE epoch observation values (Epoch: 2026-06-27T10:02:53.557Z)
Latitude
-0.00001°
Longitude
160.30453°
Altitude
342.205 km
Speed
7.706 km/s
True Right ascension
15h 06m 14s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
08:00:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
345.538 km
Perigee altitude
341.952 km
Semi-major axis
6,721.882 km
Eccentricity
0.00027
Inclination
51.6213°
RAAN
226.5608°
Arg. of periapsis
351.1614°
True anomaly
8.93855°
Mean anomaly
8.9338°
Eccentric anomaly
8.93617°
Mean motion
3.93828 °/min
Orbital period
91.41 mins
BSTAR
0.00053153
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|