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 Radar Imaging
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 + 1 Pan, 14.5 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ORBASTRO-JEN1
1 69006U 26100AC 26201.99367830 .00003308 00000-0 15453-3 0 9991
2 69006 97.4005 99.1897 0002269 235.4402 124.6619 15.20489930 11945Epoch: 2026-07-20T23:50Z
TLE epoch observation values (Epoch: 2026-07-20T23:50:53.805Z)
Latitude
-0.00005°
Longitude
162.69577°
Altitude
508.342 km
Speed
7.609 km/s
True Right ascension
06h 36m 45s
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
05:10:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.888 km
Perigee altitude
499.766 km
Semi-major axis
6,879.464 km
Eccentricity
0.00023
Inclination
97.4005°
RAAN
99.1897°
Arg. of periapsis
235.4402°
True anomaly
124.68328°
Mean anomaly
124.6619°
Eccentric anomaly
124.67259°
Mean motion
3.80374 °/min
Orbital period
94.64 mins
BSTAR
0.00015453
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-21 17:21:04.265Z | 174.776° S | 2026-07-21 17:24:04.265Z | 293.051° NW | 43.244° | 2026-07-21 17:27:04.265Z | 343.419° N |
| 6 mins | 2026-07-22 06:25:04.265Z | 356.02° N | 2026-07-22 06:28:04.265Z | 279.32° WNW | 35.626° | 2026-07-22 06:31:04.265Z | 214.225° SW |
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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