QUBE2, 69023
Orbit data source: Space-Track
QUBE2, 69023 is a payload satellite owned by ZfT (DE) in SSO that was launched on Sun, 03 May 2026 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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69023 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
NanoAvionics
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, 1.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 QUBE2
1 69023U 26100AV 26207.25897989 .00008581 00000-0 39266-3 0 9994
2 69023 97.4027 104.3849 0002169 178.6999 181.4243 15.20757354 12743Epoch: 2026-07-26T06:12Z
TLE epoch observation values (Epoch: 2026-07-26T06:12:55.862Z)
Latitude
0.00002°
Longitude
67.19266°
Altitude
508.139 km
Speed
7.609 km/s
True Right ascension
06h 57m 32s
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
16:33:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.012 km
Perigee altitude
499.028 km
Semi-major axis
6,878.657 km
Eccentricity
0.00022
Inclination
97.4027°
RAAN
104.3849°
Arg. of periapsis
178.6999°
True anomaly
181.42368°
Mean anomaly
181.4243°
Eccentric anomaly
181.42399°
Mean motion
3.80441 °/min
Orbital period
94.63 mins
BSTAR
0.00039266
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.QUBE2 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-27 06:28:26.757Z | 348.152° N | 2026-07-27 06:30:26.757Z | 294.639° NW | 33.749° | 2026-07-27 06:33:26.757Z | 218.55° SW |
| 5 mins | 2026-07-27 17:06:26.757Z | 150.728° SSE | 2026-07-27 17:08:26.757Z | 39.228° NE | 41.605° | 2026-07-27 17:11:26.757Z | 354.185° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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