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: 1 day ago
TLE from 1 day ago
0 SKYKRAFT-1A
1 55054U 23001AX 25312.62833510 .00008944 00000-0 34639-3 0 9999
2 55054 97.3558 8.4097 0010159 182.9236 177.1945 15.26350200158049Epoch: 2025-11-08T15:04Z
TLE epoch observation values (Epoch: 2025-11-08T15:04:48.152Z)
Latitude
-0.00004°
Longitude
94.15385°
Altitude
496.802 km
Speed
7.612 km/s
True Right ascension
00h 33m 38s
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
18:58:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.66 km
Perigee altitude
476.718 km
Semi-major axis
6,861.826 km
Eccentricity
0.00102
Inclination
97.3558°
RAAN
8.4097°
Arg. of periapsis
182.9236°
True anomaly
177.20019°
Mean anomaly
177.1945°
Eccentric anomaly
177.19735°
Mean motion
3.81842 °/min
Orbital period
94.28 mins
BSTAR
0.00034639
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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 | 2025-11-10 03:24:16.875Z | 134.405° SE | 2025-11-10 03:27:16.875Z | 62.335° ENE | 28.988° | 2025-11-10 03:29:16.875Z | 15.714° NNE |
| 5 mins | 2025-11-10 16:26:16.875Z | 36.236° NE | 2025-11-10 16:28:16.875Z | 112.683° SE | 36.278° | 2025-11-10 16:31:16.875Z | 174.288° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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