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 spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 ORBASTRO-JEN1
1 69006U 26100AC 26175.20726010 .00004324 00000-0 20230-3 0 9992
2 69006 97.4046 72.8902 0004017 12.5472 347.5862 15.20273136 7871Epoch: 2026-06-24T04:58Z
TLE epoch observation values (Epoch: 2026-06-24T04:58:27.272Z)
Latitude
-0.00009°
Longitude
85.90879°
Altitude
505.406 km
Speed
7.613 km/s
True Right ascension
04h 51m 33s
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
06:01:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.745 km
Perigee altitude
499.218 km
Semi-major axis
6,880.118 km
Eccentricity
0.0004
Inclination
97.4046°
RAAN
72.8902°
Arg. of periapsis
12.5472°
True anomaly
347.5763°
Mean anomaly
347.5862°
Eccentric anomaly
347.58125°
Mean motion
3.8032 °/min
Orbital period
94.66 mins
BSTAR
0.0002023
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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 | 2026-06-25 05:14:58.172Z | 51.495° ENE | 2026-06-25 05:16:58.172Z | 87.809° E | 18.529° | 2026-06-25 05:19:58.172Z | 142.518° SSE |
| 4 mins | 2026-06-25 06:49:58.172Z | 316.794° NNW | 2026-06-25 06:50:58.172Z | 291.985° WNW | 22.269° | 2026-06-25 06:53:58.172Z | 235.545° WSW |
| 5 mins | 2026-06-25 17:26:58.172Z | 185.339° SSW | 2026-06-25 17:28:58.172Z | 271.103° WNW | 41.537° | 2026-06-25 17:31:58.172Z | 339.853° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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