DRAGON GRACE 2, 100882
Orbit data source: Space-Track
DRAGON GRACE 2, 100882 is an American payload satellite in LEO that was launched on Thu, 01 Oct 2026 UTC launched from the Air Force Eastern Test Range (AFETR). 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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100882 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 DRAGON GRACE 2
1 A0882U 26226A 26276.49792087 .00005083 00000-0 10128-3 0 9996
2 A0882 51.6313 124.0722 0006914 218.1010 141.9490 15.48725660 440Epoch: 2026-10-03T11:57Z
TLE epoch observation values (Epoch: 2026-10-03T11:57:00.363Z)
Latitude
-0.00001°
Longitude
-67.38398°
Altitude
424.896 km
Speed
7.656 km/s
True Right ascension
08h 16m 17s
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
16:50:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
425.663 km
Perigee altitude
416.261 km
Semi-major axis
6,799.099 km
Eccentricity
0.00069
Inclination
51.6313°
RAAN
124.0722°
Arg. of periapsis
218.101°
True anomaly
141.9978°
Mean anomaly
141.949°
Eccentric anomaly
141.9734°
Mean motion
3.87138 °/min
Orbital period
92.99 mins
BSTAR
0.00010128
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Other satellites on launch #226 in the year 2026 (2026-10-01 UTC)
No other RSOs were in this launch
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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.DRAGON GRACE 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-03 23:16:31.925Z | 313.02° NW | 2026-10-03 23:19:31.925Z | 69.738° E | 64.66° | 2026-10-03 23:22:31.925Z | 119.806° SE |
| 4 mins | 2026-10-04 16:00:31.925Z | 182.174° SSW | 2026-10-04 16:02:31.925Z | 116.013° SE | 31.036° | 2026-10-04 16:04:31.925Z | 74.797° E |
| 4 mins | 2026-10-04 17:37:31.925Z | 289.908° WNW | 2026-10-04 17:38:31.925Z | 319.148° NNW | 30.286° | 2026-10-04 17:41:31.925Z | 33.087° NE |
| 4 mins | 2026-10-04 22:30:31.925Z | 335.921° NNW | 2026-10-04 22:32:31.925Z | 56.923° ENE | 38.66° | 2026-10-04 22:34:31.925Z | 99.419° ESE |
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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