CYBERCUBE, 69938
Orbit data source: Space-Track
CYBERCUBE, 69938 is an ESA payload satellite in SSO that was launched on Tue, 07 Jul 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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69938 intel report (Beta)
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Identifier
Orbit
Country
ESARelated business
None
Manufacturer
GMVRO/ALENSP
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
BOX, 0.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 CYBERCUBE
1 69938U 26156BX 26211.27076235 .00003796 00000-0 37437-3 0 9991
2 69938 97.7483 111.3653 0011738 76.6252 283.6276 14.92544548 3422Epoch: 2026-07-30T06:29Z
TLE epoch observation values (Epoch: 2026-07-30T06:29:53.867Z)
Latitude
0.0001°
Longitude
65.97716°
Altitude
591.129 km
Speed
7.566 km/s
True Right ascension
07h 25m 27s
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
10:38:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.198 km
Perigee altitude
578.846 km
Semi-major axis
6,965.159 km
Eccentricity
0.00117
Inclination
97.7483°
RAAN
111.3653°
Arg. of periapsis
76.6252°
True anomaly
283.49683°
Mean anomaly
283.6276°
Eccentric anomaly
283.56222°
Mean motion
3.73376 °/min
Orbital period
96.42 mins
BSTAR
0.00037437
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Other satellites on launch #156 in the year 2026 (2026-07-07 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.CYBERCUBE 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-31 05:36:24.049Z | 42.968° NE | 2026-07-31 05:39:24.049Z | 103.412° ESE | 25.553° | 2026-07-31 05:42:24.049Z | 154.694° SSE |
| 5 mins | 2026-07-31 07:12:24.049Z | 330.198° NNW | 2026-07-31 07:14:24.049Z | 293.911° NW | 20.165° | 2026-07-31 07:17:24.049Z | 244.129° WSW |
| 4 mins | 2026-07-31 16:27:24.049Z | 95.029° ESE | 2026-07-31 16:29:24.049Z | 57.822° ENE | 17.71° | 2026-07-31 16:31:24.049Z | 26.577° NE |
| 5 mins | 2026-07-31 18:02:24.049Z | 217.621° SW | 2026-07-31 18:04:24.049Z | 269.037° W | 28.278° | 2026-07-31 18:07:24.049Z | 323.95° NNW |
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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