SKYKRAFT-1A, 55054
Orbit data source: Space-Track
SKYKRAFT-1A, 55054 is a payload satellite owned by SkyKraft (AU) in SSO that was launched on Tue, 03 Jan 2023 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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55054 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
SkyKraft
Mission
Operational Commercial Communications
Bus & Motor
SKYKRAFT, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 SKYKRAFT-1A
1 55054U 23001AX 25335.63629787 .00005967 00000-0 22955-3 0 9994
2 55054 97.3536 31.0618 0011777 108.1820 252.0702 15.26700629161550Epoch: 2025-12-01T15:16Z
TLE epoch observation values (Epoch: 2025-12-01T15:16:16.135Z)
Latitude
-0.00006°
Longitude
91.26162°
Altitude
491.282 km
Speed
7.618 km/s
True Right ascension
02h 04m 14s
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
06:07:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.718 km
Perigee altitude
474.558 km
Semi-major axis
6,860.775 km
Eccentricity
0.00118
Inclination
97.3536°
RAAN
31.0618°
Arg. of periapsis
108.182°
True anomaly
251.94186°
Mean anomaly
252.0702°
Eccentric anomaly
252.00602°
Mean motion
3.8193 °/min
Orbital period
94.26 mins
BSTAR
0.00022955
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Other satellites on launch #1 in the year 2023 (2023-01-03 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.SKYKRAFT-1A 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-02 17:00:14.819Z | 356.985° N | 2025-12-02 17:02:14.819Z | 315.519° NNW | 36.507° | 2025-12-02 17:05:14.819Z | 212.522° SW |
| 4 mins | 2025-12-03 03:36:14.819Z | 133.324° SE | 2025-12-03 03:38:14.819Z | 49.281° ENE | 34.871° | 2025-12-03 03:40:14.819Z | 5.741° NNE |
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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