GEN1A-2, 69005
AKA "GEN1A-2" on Space-Track | Orbit data source: Space-Track
GEN1A-2, 69005 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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69005 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: 22 hours ago
TLE from 22 hours ago
0 GEN1A-2
1 69005U 26100AB 26237.25982462 .00003011 00000-0 14010-3 0 9991
2 69005 97.3938 133.7941 0006521 124.1387 236.0468 15.20689872 17318Epoch: 2026-08-25T06:14Z
TLE epoch observation values (Epoch: 2026-08-25T06:14:08.847Z)
Latitude
0.00001°
Longitude
66.7275°
Altitude
509.359 km
Speed
7.608 km/s
True Right ascension
08h 55m 10s
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
19:51:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.209 km
Perigee altitude
496.237 km
Semi-major axis
6,878.86 km
Eccentricity
0.00065
Inclination
97.3938°
RAAN
133.7941°
Arg. of periapsis
124.1387°
True anomaly
235.98484°
Mean anomaly
236.0468°
Eccentric anomaly
236.01582°
Mean motion
3.80424 °/min
Orbital period
94.63 mins
BSTAR
0.0001401
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-26 06:30:08.416Z | 340.426° N | 2026-08-26 06:32:08.416Z | 273.412° WNW | 32.115° | 2026-08-26 06:35:08.416Z | 217.398° SW |
| 5 mins | 2026-08-26 17:07:08.416Z | 157.174° SSE | 2026-08-26 17:09:08.416Z | 112.944° SE | 42.798° | 2026-08-26 17:12:08.416Z | 354.166° N |
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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