GEMS2-AMETHYST, 68505
Orbit data source: Space-Track
GEMS2-AMETHYST, 68505 is an American payload satellite in SSO that was launched on Mon, 30 Mar 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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68505 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
OMS
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: 2 days ago
TLE from 2 days ago
0 GEMS2-AMETHYST
1 68505U 26067CT 26171.38445257 .00003059 00000-0 31367-3 0 9990
2 68505 97.7602 129.4835 0006731 46.7420 313.4359 14.91163934 12191Epoch: 2026-06-20T09:13Z
TLE epoch observation values (Epoch: 2026-06-20T09:13:36.702Z)
Latitude
-0.00002°
Longitude
82.48073°
Altitude
594.12 km
Speed
7.565 km/s
True Right ascension
08h 37m 56s
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
16:35:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
596.016 km
Perigee altitude
586.634 km
Semi-major axis
6,969.462 km
Eccentricity
0.00067
Inclination
97.7602°
RAAN
129.4835°
Arg. of periapsis
46.742°
True anomaly
313.37986°
Mean anomaly
313.4359°
Eccentric anomaly
313.40788°
Mean motion
3.7303 °/min
Orbital period
96.51 mins
BSTAR
0.00031367
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.GEMS2-AMETHYST 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:06:22.203Z | 12.555° NNE | 2026-06-22 10:10:22.203Z | 191.659° SSW | 43.007° | 2026-06-22 10:13:22.203Z | 193.285° SSW |
| 6 mins | 2026-06-22 20:57:22.203Z | 144.156° SSE | 2026-06-22 20:59:22.203Z | 102.908° ESE | 37.753° | 2026-06-22 21:03:22.203Z | 358.815° 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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