GRAVITAS, 68495
Orbit data source: Space-Track
GRAVITAS, 68495 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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68495 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
K2SP
Mission
Operational spacecraft
Bus & Motor
GRAVITAS, Unknown motor
Mass
2,000 kg wet, 1,800 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 GRAVITAS
1 68495U 26067CH 26167.00003472 -.00057108 00000-0 -10611-1 0 9994
2 68495 97.7615 123.2245 0003779 40.0776 261.6250 14.65561586 4832Epoch: 2026-06-16T00:00Z
TLE epoch observation values (Epoch: 2026-06-16T00:00:02.999Z)
Latitude
-57.72127°
Longitude
-128.6731°
Altitude
698.017 km
Speed
7.506 km/s
True Right ascension
09h 02m 28s
True Declination
-57° 33' 52"
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
15:17:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
674.991 km
Perigee altitude
669.663 km
Semi-major axis
7,050.464 km
Eccentricity
0.00038
Inclination
97.7615°
RAAN
123.2245°
Arg. of periapsis
40.0776°
True anomaly
261.58216°
Mean anomaly
261.625°
Eccentric anomaly
261.60358°
Mean motion
3.6662 °/min
Orbital period
98.19 mins
BSTAR
-0.010611
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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.GRAVITAS 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 09:16:06.843Z | 33.699° NE | 2026-06-22 09:20:06.843Z | 97.715° ESE | 28.206° | 2026-06-22 09:24:06.843Z | 159.907° S |
| 5 mins | 2026-06-22 10:55:06.843Z | 328.772° NNW | 2026-06-22 10:57:06.843Z | 293.557° NW | 22.107° | 2026-06-22 11:00:06.843Z | 245.629° WSW |
| 6 mins | 2026-06-22 20:19:06.843Z | 118.619° SE | 2026-06-22 20:22:06.843Z | 63.084° ENE | 25.66° | 2026-06-22 20:25:06.843Z | 15.219° NNE |
| 5 mins | 2026-06-22 21:57:06.843Z | 226.985° WSW | 2026-06-22 21:59:06.843Z | 265.33° W | 23.873° | 2026-06-22 22:02:06.843Z | 315.083° 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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