DRAGON GRACE 2, 100882
Orbit data source: Space-Track
DRAGON GRACE 2, 100882 is a payload satellite owned by SpaceX (US) in LEO that was launched on Thu, 01 Oct 2026 UTC via an FALCON 9 launch vehicle 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
Manufacturer
SpaceX
Mission
Operational spacecraft
Bus & Motor
DRAGON CM, Unknown motor
Mass
~13,055 kg wet, ~9,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
FRUST + CYL, 2.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 DRAGON GRACE 2
1 A0882U 26226A 26286.82178356 .00006288 00000-0 12278-3 0 9997
2 A0882 51.6323 73.0088 0006721 259.4454 100.5777 15.48855494 1567Epoch: 2026-10-13T19:43Z
TLE epoch observation values (Epoch: 2026-10-13T19:43:22.099Z)
Latitude
-0.00005°
Longitude
114.78633°
Altitude
421.655 km
Speed
7.659 km/s
True Right ascension
04h 52m 02s
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
14:59:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
425.151 km
Perigee altitude
416.013 km
Semi-major axis
6,798.719 km
Eccentricity
0.00067
Inclination
51.6323°
RAAN
73.0088°
Arg. of periapsis
259.4454°
True anomaly
100.6534°
Mean anomaly
100.5777°
Eccentric anomaly
100.61555°
Mean motion
3.87171 °/min
Orbital period
92.98 mins
BSTAR
0.00012278
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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 | 2026-10-15 12:09:50.156Z | 219.312° SW | 2026-10-15 12:12:50.156Z | 107.735° ESE | 59.648° | 2026-10-15 12:15:50.156Z | 58.223° ENE |
| 5 mins | 2026-10-15 18:40:50.156Z | 314.618° NW | 2026-10-15 18:42:50.156Z | 71.625° E | 70.944° | 2026-10-15 18:45:50.156Z | 122.082° SE |
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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