KUIPER-00560, 69623
Orbit data source: Space-Track
KUIPER-00560, 69623 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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69623 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-00560
1 69623U 26140AH 26178.50002315 .00022959 00000-0 60380-3 0 9996
2 69623 51.8796 348.8199 0008692 231.9107 12.4081 15.38444174 2395Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-45.35029°
Longitude
125.37704°
Altitude
460.144 km
Speed
7.64 km/s
True Right ascension
14h 43m 59s
True Declination
-45° 10' 15"
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
09:24:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.112 km
Perigee altitude
445.24 km
Semi-major axis
6,829.313 km
Eccentricity
0.00087
Inclination
51.8796°
RAAN
348.8199°
Arg. of periapsis
231.9107°
True anomaly
12.42952°
Mean anomaly
12.4081°
Eccentric anomaly
12.41881°
Mean motion
3.84572 °/min
Orbital period
93.61 mins
BSTAR
0.0006038
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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-00560 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 | 2026-06-28 13:37:30.209Z | 200.572° SSW | 2026-06-28 13:39:30.209Z | 146.381° SSE | 34.252° | 2026-06-28 13:42:30.209Z | 67.276° ENE |
| 4 mins | 2026-06-28 15:15:30.209Z | 288.53° WNW | 2026-06-28 15:17:30.209Z | 341.1° N | 24.75° | 2026-06-28 15:19:30.209Z | 25.538° NE |
| 5 mins | 2026-06-28 20:10:30.209Z | 324.821° NNW | 2026-06-28 20:12:30.209Z | 38.329° NE | 38.581° | 2026-06-28 20:15:30.209Z | 110.54° ESE |
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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