GEN1A-1, 69004
AKA "GEN1A-1" on Space-Track | Orbit data source: Space-Track
GEN1A-1, 69004 is a payload satellite owned by Lynk (US) 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
Manufacturer
Lynk
Mission
Operational Commercial Communications
Bus & Motor
LYNK SHANNON, Unknown motor
Mass
~85 kg wet, ~85 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.650 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 GEN1A-1
1 69004U 26100AA 26220.68725114 .00001416 00000-0 68090-4 0 9993
2 69004 97.3979 117.5295 0004300 165.5484 194.5875 15.20420353 14790Epoch: 2026-08-08T16:29Z
TLE epoch observation values (Epoch: 2026-08-08T16:29:38.498Z)
Latitude
-0.00004°
Longitude
-87.07592°
Altitude
510.528 km
Speed
7.607 km/s
True Right ascension
07h 50m 07s
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
21:26:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.495 km
Perigee altitude
498.578 km
Semi-major axis
6,879.674 km
Eccentricity
0.00043
Inclination
97.3979°
RAAN
117.5295°
Arg. of periapsis
165.5484°
True anomaly
194.5751°
Mean anomaly
194.5875°
Eccentric anomaly
194.5813°
Mean motion
3.80357 °/min
Orbital period
94.65 mins
BSTAR
0.00006809
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-09 17:54:55.939Z | 229.657° WSW | 2026-08-09 17:55:55.939Z | 254.633° W | 23.791° | 2026-08-09 17:58:55.939Z | 318.334° NNW |
| 4 mins | 2026-08-10 05:24:55.939Z | 58.719° ENE | 2026-08-10 05:26:55.939Z | 109.86° ESE | 22.803° | 2026-08-10 05:28:55.939Z | 147.935° SSE |
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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