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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.

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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, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 QUBE
1 60476U 24149J   26127.20790927  .00019802  00000-0  41617-3 0  9999
2 60476  97.3768 212.9148 0002232  55.5515 304.5944 15.45365621 96133
Epoch: 2026-05-07T04:59Z
TLE epoch observation values (Epoch: 2026-05-07T04:59:23.360Z)
Latitude
-0.00011°
Longitude
-86.98987°
Altitude
432.567 km
Speed
7.653 km/s
True Right ascension
14h 11m 39s
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
23:28:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.754 km
Perigee altitude
425.716 km
Semi-major axis
6,805.372 km
Eccentricity
0.00022
Inclination
97.3768°
RAAN
212.9148°
Arg. of periapsis
55.5515°
True anomaly
304.57334°
Mean anomaly
304.5944°
Eccentric anomaly
304.58387°
Mean motion
3.86603 °/min
Orbital period
93.12 mins
BSTAR
0.00041617
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