Showing default

QUBE, 60476

Orbit data source: Space-Track

QUBE, 60476 is a payload satellite owned by ZfT (DE) in SSO that was launched on Fri, 16 Aug 2024 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
60476, 2024-149J
Orbit
SSO
Country
Flag of DEDE / GER
Related business
Manufacturer
ZfT
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 QUBE
1 60476U 24149J   26219.74412569  .00015854  00000-0  28805-3 0  9990
2 60476  97.3749 307.2567 0002747  74.8963 285.2592 15.49636535110441
Epoch: 2026-08-07T17:51Z
TLE epoch observation values (Epoch: 2026-08-07T17:51:32.459Z)
Latitude
-0.00003°
Longitude
83.10603°
Altitude
420.429 km
Speed
7.659 km/s
True Right ascension
20h 29m 01s
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
15:42:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.58 km
Perigee altitude
412.848 km
Semi-major axis
6,792.851 km
Eccentricity
0.00027
Inclination
97.3749°
RAAN
307.2567°
Arg. of periapsis
74.8963°
True anomaly
285.22883°
Mean anomaly
285.2592°
Eccentric anomaly
285.24401°
Mean motion
3.87673 °/min
Orbital period
92.86 mins
BSTAR
0.00028805
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
|