KUIPER-00561, 69624
Orbit data source: Space-Track
KUIPER-00561, 69624 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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69624 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: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00561
1 69624U 26140AJ 26178.50002315 .00024605 00000-0 65064-3 0 9991
2 69624 51.8830 348.8343 0007962 232.2833 7.1376 15.38238962 2603Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-42.83594°
Longitude
119.54962°
Altitude
460.12 km
Speed
7.639 km/s
True Right ascension
14h 20m 41s
True Declination
-42° 39' 25"
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
10:52:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.22 km
Perigee altitude
446.344 km
Semi-major axis
6,829.919 km
Eccentricity
0.0008
Inclination
51.883°
RAAN
348.8343°
Arg. of periapsis
232.2833°
True anomaly
7.14895°
Mean anomaly
7.1376°
Eccentric anomaly
7.14327°
Mean motion
3.84521 °/min
Orbital period
93.62 mins
BSTAR
0.00065064
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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-00561 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 13:37:58.800Z | 209.308° SW | 2026-06-28 13:40:58.800Z | 150.088° SSE | 34.826° | 2026-06-28 13:43:58.800Z | 66.943° ENE |
| 4 mins | 2026-06-28 15:16:58.800Z | 288.041° WNW | 2026-06-28 15:18:58.800Z | 338.702° N | 24.461° | 2026-06-28 15:20:58.800Z | 24.218° NE |
| 5 mins | 2026-06-28 20:11:58.800Z | 322.934° NNW | 2026-06-28 20:13:58.800Z | 29.768° NE | 39.172° | 2026-06-28 20:16:58.800Z | 111.034° 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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