Showing default

HUBBLE 7, 64592

Orbit data source: Space-Track

HUBBLE 7, 64592 is an American payload satellite in SSO that was launched on Mon, 23 Jun 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
64592, 2025-135BS
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Endurosat
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
2025-06-23 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 1.0 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 HUBBLE 7
1 64592U 25135BS  26224.56114435  .00000422  00000-0  45285-4 0  9993
2 64592  97.7796 338.6600 0003829 139.0490 221.1018 14.93722243 62322
Epoch: 2026-08-12T13:28Z
TLE epoch observation values (Epoch: 2026-08-12T13:28:02.871Z)
Latitude
-0.00004°
Longitude
175.63473°
Altitude
591.396 km
Speed
7.563 km/s
True Right ascension
22h 34m 38s
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
16:54:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.024 km
Perigee altitude
580.693 km
Semi-major axis
6,961.496 km
Eccentricity
0.00038
Inclination
97.7796°
RAAN
338.66°
Arg. of periapsis
139.049°
True anomaly
221.07297°
Mean anomaly
221.1018°
Eccentric anomaly
221.08738°
Mean motion
3.73671 °/min
Orbital period
96.34 mins
BSTAR
0.000045285
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
|