GEN1A-2, 69005
AKA "GEN1A-2" on Space-Track | Orbit data source: Space-Track
GEN1A-2, 69005 is an American payload satellite 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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69005 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
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 GEN1A-2
1 69005U 26100AB 26175.20227339 .00003305 00000-0 15506-3 0 9999
2 69005 97.4031 72.8835 0005362 14.9999 345.1394 15.20338326 7881Epoch: 2026-06-24T04:51Z
TLE epoch observation values (Epoch: 2026-06-24T04:51:16.420Z)
Latitude
-0.00009°
Longitude
87.70222°
Altitude
504.342 km
Speed
7.614 km/s
True Right ascension
04h 51m 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
05:58:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.474 km
Perigee altitude
498.096 km
Semi-major axis
6,879.922 km
Eccentricity
0.00054
Inclination
97.4031°
RAAN
72.8835°
Arg. of periapsis
14.9999°
True anomaly
345.12363°
Mean anomaly
345.1394°
Eccentric anomaly
345.13152°
Mean motion
3.80336 °/min
Orbital period
94.65 mins
BSTAR
0.00015506
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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.GEN1A-2 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-25 05:08:07.844Z | 59.277° ENE | 2026-06-25 05:10:07.844Z | 95.201° ESE | 15.648° | 2026-06-25 05:12:07.844Z | 130.025° SE |
| 5 mins | 2026-06-25 06:42:07.844Z | 333.624° NNW | 2026-06-25 06:44:07.844Z | 281.786° WNW | 25.92° | 2026-06-25 06:47:07.844Z | 227.395° WSW |
| 6 mins | 2026-06-25 17:19:07.844Z | 172.235° S | 2026-06-25 17:22:07.844Z | 325.841° NNW | 42.021° | 2026-06-25 17:25:07.844Z | 345.552° 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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