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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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: 11 hours ago
TLE from 11 hours ago
0 SKYKRAFT-1A
1 55054U 23001AX 26068.71064616 .00008177 00000-0 30069-3 0 9992
2 55054 97.3349 127.6290 0011277 121.5092 238.7251 15.28083228176529Epoch: 2026-03-09T17:03Z
TLE epoch observation values (Epoch: 2026-03-09T17:03:19.828Z)
Latitude
-0°
Longitude
64.3967°
Altitude
488.669 km
Speed
7.618 km/s
True Right ascension
08h 30m 30s
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
08:28:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.227 km
Perigee altitude
470.762 km
Semi-major axis
6,856.632 km
Eccentricity
0.00113
Inclination
97.3349°
RAAN
127.629°
Arg. of periapsis
121.5092°
True anomaly
238.61473°
Mean anomaly
238.7251°
Eccentric anomaly
238.66991°
Mean motion
3.82276 °/min
Orbital period
94.17 mins
BSTAR
0.00030069
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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 | 2026-03-10 17:11:54.579Z | 342.988° N | 2026-03-10 17:13:54.579Z | 287.828° WNW | 30.161° | 2026-03-10 17:16:54.579Z | 221.396° SW |
| 5 mins | 2026-03-11 03:46:54.579Z | 151.524° SSE | 2026-03-11 03:48:54.579Z | 28.344° NE | 40.769° | 2026-03-11 03:51:54.579Z | 353.463° N |
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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