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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60476 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
ZfT
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 QUBE
1 60476U 24149J 26221.81043328 .00019891 00000-0 35979-3 0 9999
2 60476 97.3758 309.3698 0002587 68.8943 291.2585 15.49715097110767Epoch: 2026-08-09T19:27Z
TLE epoch observation values (Epoch: 2026-08-09T19:27:01.435Z)
Latitude
0.00002°
Longitude
59.31174°
Altitude
420.053 km
Speed
7.659 km/s
True Right ascension
20h 37m 28s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:35:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.241 km
Perigee altitude
412.727 km
Semi-major axis
6,792.621 km
Eccentricity
0.00026
Inclination
97.3758°
RAAN
309.3698°
Arg. of periapsis
68.8943°
True anomaly
291.23087°
Mean anomaly
291.2585°
Eccentric anomaly
291.24468°
Mean motion
3.87692 °/min
Orbital period
92.86 mins
BSTAR
0.00035979
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.QUBE Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-10 06:26:40.826Z | 217.298° SW | 2026-08-10 06:27:40.826Z | 248.007° W | 27.026° | 2026-08-10 06:30:40.826Z | 325.521° NNW |
| 4 mins | 2026-08-10 19:15:40.826Z | 339.242° N | 2026-08-10 19:17:40.826Z | 275.343° WNW | 27.736° | 2026-08-10 19:19:40.826Z | 227.259° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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