KUIPER-00528, 69603
Orbit data source: Space-Track
KUIPER-00528, 69603 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Wed, 17 Jun 2026 UTC via an ARIANE 64 launch vehicle from the French Guiana (FRGUI). 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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69603 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational spacecraft
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00528
1 69603U 26140M 26178.50002315 .00021171 00000-0 58400-3 0 9999
2 69603 51.8803 348.9221 0004516 292.1935 261.6771 15.37041534 1304Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-10.97123°
Longitude
82.00099°
Altitude
458.143 km
Speed
7.638 km/s
True Right ascension
11h 50m 29s
True Declination
-10° 54' 16"
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
09:23:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.415 km
Perigee altitude
452.243 km
Semi-major axis
6,833.466 km
Eccentricity
0.00045
Inclination
51.8803°
RAAN
348.9221°
Arg. of periapsis
292.1935°
True anomaly
261.6259°
Mean anomaly
261.6771°
Eccentric anomaly
261.6515°
Mean motion
3.84221 °/min
Orbital period
93.7 mins
BSTAR
0.000584
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Other satellites on launch #140 in the year 2026 (2026-06-17 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.KUIPER-00528 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 | 2026-06-28 13:51:18.708Z | 219.331° SW | 2026-06-28 13:54:18.708Z | 177.284° S | 39.337° | 2026-06-28 13:57:18.708Z | 61.446° ENE |
| 4 mins | 2026-06-28 15:31:18.708Z | 305.453° NW | 2026-06-28 15:32:18.708Z | 329.599° NNW | 21.318° | 2026-06-28 15:35:18.708Z | 29.834° NE |
| 5 mins | 2026-06-28 20:26:18.708Z | 317.413° NNW | 2026-06-28 20:28:18.708Z | 86.029° E | 42.014° | 2026-06-28 20:31:18.708Z | 121.638° SE |
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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