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: 22 hours ago
TLE from 22 hours ago
0 SKYKRAFT-1
1 55041U 23001AJ 25296.87912274 .00034295 00000-0 70081-3 0 9997
2 55041 97.3549 2.7677 0006457 200.2675 159.8319 15.46061393156306Epoch: 2025-10-23T21:05Z
TLE epoch observation values (Epoch: 2025-10-23T21:05:56.204Z)
Latitude
-0.00004°
Longitude
13.75147°
Altitude
435.515 km
Speed
7.648 km/s
True Right ascension
00h 11m 04s
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
13:57:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.583 km
Perigee altitude
420.797 km
Semi-major axis
6,803.327 km
Eccentricity
0.00065
Inclination
97.3549°
RAAN
2.7677°
Arg. of periapsis
200.2675°
True anomaly
159.85739°
Mean anomaly
159.8319°
Eccentric anomaly
159.84465°
Mean motion
3.86777 °/min
Orbital period
93.08 mins
BSTAR
0.00070081
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-25 04:18:03.653Z | 146.98° SSE | 2025-10-25 04:20:03.653Z | 104.729° ESE | 35.24° | 2025-10-25 04:23:03.653Z | 2.45° NNE |
| 4 mins | 2025-10-25 17:10:03.653Z | 32.585° NE | 2025-10-25 17:12:03.653Z | 123.819° SE | 37.126° | 2025-10-25 17:14:03.653Z | 173.437° 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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