ORBASTRO-JEN1, 69006
Orbit data source: Space-Track
ORBASTRO-JEN1, 69006 is a payload satellite owned by OrbAstro (UK) 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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69006 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
OrbAstro
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 14.5 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ORBASTRO-JEN1
1 69006U 26100AC 26220.68371753 .00002321 00000-0 10945-3 0 9992
2 69006 97.3988 117.5403 0008824 169.6342 190.5077 15.20447110 14785Epoch: 2026-08-08T16:24Z
TLE epoch observation values (Epoch: 2026-08-08T16:24:33.194Z)
Latitude
-0.00003°
Longitude
-85.78954°
Altitude
513.555 km
Speed
7.604 km/s
True Right ascension
07h 50m 09s
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
21:25:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.526 km
Perigee altitude
495.385 km
Semi-major axis
6,879.593 km
Eccentricity
0.00088
Inclination
97.3988°
RAAN
117.5403°
Arg. of periapsis
169.6342°
True anomaly
190.48928°
Mean anomaly
190.5077°
Eccentric anomaly
190.49849°
Mean motion
3.80364 °/min
Orbital period
94.65 mins
BSTAR
0.00010945
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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.ORBASTRO-JEN1 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 | 2026-08-09 17:49:12.176Z | 213.391° SW | 2026-08-09 17:51:12.176Z | 264.117° W | 27.061° | 2026-08-09 17:54:12.176Z | 324.424° NNW |
| 4 mins | 2026-08-10 05:20:12.176Z | 68.223° E | 2026-08-10 05:21:12.176Z | 91.63° ESE | 20.615° | 2026-08-10 05:24:12.176Z | 147.764° SSE |
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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