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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Edit Public Description
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, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 QUBE
1 60476U 24149J 25291.18317648 .00028828 00000-0 85892-3 0 9993
2 60476 97.4012 9.9137 0002754 46.8077 313.3396 15.34638143 65194Epoch: 2025-10-18T04:23Z
TLE epoch observation values (Epoch: 2025-10-18T04:23:46.447Z)
Latitude
-0.00002°
Longitude
-82.94768°
Altitude
463.813 km
Speed
7.635 km/s
True Right ascension
00h 39m 39s
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
05:49:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.825 km
Perigee altitude
457.059 km
Semi-major axis
6,837.079 km
Eccentricity
0.00028
Inclination
97.4012°
RAAN
9.9137°
Arg. of periapsis
46.8077°
True anomaly
313.31664°
Mean anomaly
313.3396°
Eccentric anomaly
313.32812°
Mean motion
3.83917 °/min
Orbital period
93.77 mins
BSTAR
0.00085892
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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 | 2025-10-18 17:29:18.841Z | 48.616° ENE | 2025-10-18 17:31:18.841Z | 86.592° E | 18.89° | 2025-10-18 17:33:18.841Z | 131.91° SE |
| 5 mins | 2025-10-19 05:34:18.841Z | 180.025° SSW | 2025-10-19 05:36:18.841Z | 243.148° WSW | 42.341° | 2025-10-19 05:39:18.841Z | 341.007° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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