SKYKRAFT-1, 55041
Orbit data source: Space-Track
SKYKRAFT-1, 55041 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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55041 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
SkyKraft
Mission
Operational Commercial Technology
Bus & Motor
SKYKRAFT CARRIER, AOCS
Mass
~100 kg wet, ~100 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: 7 hours ago
TLE from 7 hours ago
0 SKYKRAFT-1
1 55041U 23001AJ 25288.65764574 .00033613 00000-0 70178-3 0 9992
2 55041 97.3567 354.4317 0005989 232.1320 127.9388 15.45438969155031Epoch: 2025-10-15T15:47Z
TLE epoch observation values (Epoch: 2025-10-15T15:47:00.591Z)
Latitude
-0.00003°
Longitude
93.25067°
Altitude
435.724 km
Speed
7.649 km/s
True Right ascension
23h 37m 43s
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
16:56:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.094 km
Perigee altitude
422.943 km
Semi-major axis
6,805.155 km
Eccentricity
0.0006
Inclination
97.3567°
RAAN
354.4317°
Arg. of periapsis
232.132°
True anomaly
127.9929°
Mean anomaly
127.9388°
Eccentric anomaly
127.96585°
Mean motion
3.86622 °/min
Orbital period
93.11 mins
BSTAR
0.00070178
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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-1 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 | 2025-10-16 04:20:39.339Z | 153.403° SSE | 2025-10-16 04:23:39.339Z | 58.384° ENE | 39.651° | 2025-10-16 04:26:39.339Z | 356.646° N |
| 4 mins | 2025-10-16 17:13:39.339Z | 29.986° NE | 2025-10-16 17:14:39.339Z | 61.165° ENE | 39.226° | 2025-10-16 17:17:39.339Z | 180.3° SSW |
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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