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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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Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/55041?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/55041?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

55041, 2023-001AJ

Orbit

SSO

Country

AU / AUS

Related business

Manufacturer

SkyKraft

Mission

Operational Commercial Technology

Bus & Motor

SKYKRAFT CARRIER, AOCS

Mass

~100 kg wet, ~100 kg dry

Launch date (UTC)

2023-01-03 (3 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.3 m

Radar Cross Section

0.065 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 SKYKRAFT-1
1 55041U 23001AJ  26120.53396801  .00044461  00000-0  50106-3 0  9991
2 55041  97.3209 195.9980 0003849 223.0429 137.0529 15.62412839185602

Epoch: 2026-04-30T12:48Z

TLE epoch observation values (Epoch: 2026-04-30T12:48:54.836Z)

Latitude

0.00004°

Longitude

145.29031°

Altitude

385.745 km

Speed

7.677 km/s

True Right ascension

13h 03m 59s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

10:01:41

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

380.196 km

Perigee altitude

374.995 km

Semi-major axis

6,755.733 km

Eccentricity

0.00038

Inclination

97.3209°

RAAN

195.998°

Arg. of periapsis

223.0429°

True anomaly

137.08294°

Mean anomaly

137.0529°

Eccentric anomaly

137.06792°

Mean motion

3.90872 °/min

Orbital period

92.1 mins

BSTAR

0.00050106

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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)

FLOCK 4Y 34, 55082 (Decayed)

NSL-2, 55067 (Decayed)

SPACEBEE-166, 55092 (Decayed)

OBJECT H, 55016

CONNECTA T1.2, 55012

LYNK TOWER 3, 55046

TAUSAT-2, 55073 (Decayed)

ION SCV-007, 55060

ASTROCAST-0402, 55109

OBJECT A, 55009

OBJECT-DD, 55108 (Decayed)

ASTROCAST-0404, 55112

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

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.
4 mins	2026-05-01 04:20:00.851Z	115.022° SE	2026-05-01 04:22:00.851Z	71.655° E	17.202°	2026-05-01 04:24:00.851Z	27.253° NE

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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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Check out SKYKRAFT-1, 55041 on other resources

View SKYKRAFT-1, 55041 on NASA - NSSDCA Website

View SKYKRAFT-1, 55041 on Heavens-Above

View SKYKRAFT-1, 55041 on Keep Track

View SKYKRAFT-1, 55041 on Celestrak

View SKYKRAFT-1, 55041 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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