GEN1A-1, 69004
AKA "GEN1A-1" on Space-Track | Orbit data source: Space-Track
GEN1A-1, 69004 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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69004 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: 10 hours ago
TLE from 10 hours ago
0 GEN1A-1
1 69004U 26100AA 26168.62445897 .00002187 00000-0 10421-3 0 9995
2 69004 97.4047 66.4281 0005037 33.7731 326.3824 15.20156020 6880Epoch: 2026-06-17T14:59Z
TLE epoch observation values (Epoch: 2026-06-17T14:59:13.255Z)
Latitude
-0.00002°
Longitude
-64.25659°
Altitude
505.573 km
Speed
7.613 km/s
True Right ascension
04h 25m 42s
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
12:12:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.801 km
Perigee altitude
498.869 km
Semi-major axis
6,880.472 km
Eccentricity
0.0005
Inclination
97.4047°
RAAN
66.4281°
Arg. of periapsis
33.7731°
True anomaly
326.35043°
Mean anomaly
326.3824°
Eccentric anomaly
326.36642°
Mean motion
3.80291 °/min
Orbital period
94.66 mins
BSTAR
0.00010421
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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-1 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 | 2026-06-18 05:46:25.441Z | 27.047° NE | 2026-06-18 05:49:25.441Z | 112.87° SE | 37.021° | 2026-06-18 05:52:25.441Z | 174.471° S |
| 4 mins | 2026-06-18 16:25:25.441Z | 104.09° ESE | 2026-06-18 16:27:25.441Z | 62.249° ENE | 18.709° | 2026-06-18 16:29:25.441Z | 25.974° NE |
| 4 mins | 2026-06-18 17:59:25.441Z | 230.648° WSW | 2026-06-18 18:00:25.441Z | 253.358° W | 21.518° | 2026-06-18 18:03:25.441Z | 315.32° NNW |
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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