ORION, 54257 (Decayed)
Orbit data source: Space-Track
ORION, 54257 was a payload satellite owned by NASA JSC (US) that was launched on Wed, 16 Nov 2022 UTC via an SLS BLOCK 1 launch vehicle from the Air Force Eastern Test Range (AFETR).
Artemis I was a successful uncrewed flight test launched on November 16, 2022, serving as the inaugural mission of NASA's Artemis program. It tested the powerful Space Launch System (SLS) rocket and the Orion spacecraft to ensure safe, sustainable human exploration of the Moon and future deep-space missions to Mars.
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54257 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LM KSC
Mission
Decayed Civil Spaceship
Bus & Motor
ORION, Unknown motor
Mass
26,048 kg wet, 9,400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cone, 2.5 m
Radar Cross Section
13.354 m²
Expand to show TLE details & historyLast TLE update: N/A
TLE epoch observation values
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
True Right ascension
Unknown
True Declination
Unknown
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
13:03:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
Unknown
Perigee altitude
Unknown
Semi-major axis
Unknown
Eccentricity
Unknown
Inclination
Unknown
RAAN
Unknown
Arg. of periapsis
Unknown
True anomaly
Unknown
Mean anomaly
Unknown
Eccentric anomaly
Unknown
Mean motion
Unknown
Orbital period
Unknown
BSTAR
Unknown
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Other satellites on launch #156 in the year 2022 (2022-11-16 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.ORION Visibility
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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. |
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| This satellite is decayed. |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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