SKYKRAFT-1C, 55061
Orbit data source: Space-Track
SKYKRAFT-1C, 55061 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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55061 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-1C
1 55061U 23001BE 26068.70960345 .00004538 00000-0 18809-3 0 9998
2 55061 97.3326 124.5476 0011974 132.0782 228.1477 15.24327539176324Epoch: 2026-03-09T17:01Z
TLE epoch observation values (Epoch: 2026-03-09T17:01:49.738Z)
Latitude
0.00009°
Longitude
61.6917°
Altitude
501.4 km
Speed
7.611 km/s
True Right ascension
08h 18m 11s
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
497.986 km
Perigee altitude
481.539 km
Semi-major axis
6,867.899 km
Eccentricity
0.0012
Inclination
97.3326°
RAAN
124.5476°
Arg. of periapsis
132.0782°
True anomaly
228.0456°
Mean anomaly
228.1477°
Eccentric anomaly
228.09664°
Mean motion
3.81336 °/min
Orbital period
94.41 mins
BSTAR
0.00018809
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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-1C 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-10 15:39:54.062Z | 51.518° ENE | 2026-03-10 15:41:54.062Z | 87.209° E | 17.166° | 2026-03-10 15:43:54.062Z | 128.059° SE |
| 4 mins | 2026-03-10 17:13:54.062Z | 332.097° NNW | 2026-03-10 17:15:54.062Z | 286.132° WNW | 22.212° | 2026-03-10 17:17:54.062Z | 243.157° WSW |
| 5 mins | 2026-03-11 03:49:54.062Z | 178.851° S | 2026-03-11 03:51:54.062Z | 253.889° W | 43.331° | 2026-03-11 03:54:54.062Z | 342.238° 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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