KUWAITSAT-1, 55103
Orbit data source: Space-Track
KUWAITSAT-1, 55103 is a payload satellite owned by Kuwait U. (KW) 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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55103 intel report (Beta)
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Identifier
Orbit
Country
KW / KWTRelated business
Manufacturer
Kuwait U.
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KUWAITSAT-1
1 55103U 23001CY 26166.13804010 .00021761 00000-0 39467-3 0 9997
2 55103 97.3252 236.9072 0009280 88.0763 272.1551 15.49575450192273Epoch: 2026-06-15T03:18Z
TLE epoch observation values (Epoch: 2026-06-15T03:18:46.664Z)
Latitude
-0.00004°
Longitude
-76.21596°
Altitude
420.868 km
Speed
7.659 km/s
True Right ascension
15h 47m 37s
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
00:01:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
421.194 km
Perigee altitude
408.586 km
Semi-major axis
6,793.027 km
Eccentricity
0.00093
Inclination
97.3252°
RAAN
236.9072°
Arg. of periapsis
88.0763°
True anomaly
272.04883°
Mean anomaly
272.1551°
Eccentric anomaly
272.10197°
Mean motion
3.87657 °/min
Orbital period
92.87 mins
BSTAR
0.00039467
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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.KUWAITSAT-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 | 2026-06-15 17:48:51.181Z | 1.41° NNE | 2026-06-15 17:51:51.181Z | 256.516° W | 38.374° | 2026-06-15 17:53:51.181Z | 209.051° SW |
| 4 mins | 2026-06-16 04:15:51.181Z | 116.87° SE | 2026-06-16 04:17:51.181Z | 55.446° ENE | 23.877° | 2026-06-16 04:19:51.181Z | 14.633° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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