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 Commercial Weather
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 2.0 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 GEMS2-AMETHYST
1 68505U 26067CT 26193.86265135 .00001828 00000-0 18890-3 0 9990
2 68505 97.7614 151.6004 0004606 338.7770 21.3257 14.91333614 15548Epoch: 2026-07-12T20:42Z
TLE epoch observation values (Epoch: 2026-07-12T20:42:13.076Z)
Latitude
-0.00001°
Longitude
-89.70951°
Altitude
593.825 km
Speed
7.565 km/s
True Right ascension
10h 06m 24s
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
21:27:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.006 km
Perigee altitude
587.586 km
Semi-major axis
6,968.933 km
Eccentricity
0.00046
Inclination
97.7614°
RAAN
151.6004°
Arg. of periapsis
338.777°
True anomaly
21.34491°
Mean anomaly
21.3257°
Eccentric anomaly
21.3353°
Mean motion
3.73073 °/min
Orbital period
96.5 mins
BSTAR
0.0001889
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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 | 2026-07-13 10:08:46.630Z | 10.83° NNE | 2026-07-13 10:12:46.630Z | 225.882° WSW | 44.51° | 2026-07-13 10:15:46.630Z | 196.189° SSW |
| 6 mins | 2026-07-13 20:59:46.630Z | 148.506° SSE | 2026-07-13 21:02:46.630Z | 52.174° ENE | 40.009° | 2026-07-13 21:05:46.630Z | 357.865° 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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