KUIPER-00544, 69613
Orbit data source: Space-Track
KUIPER-00544, 69613 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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69613 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-00544
1 69613U 26140X 26178.50002315 .00022076 00000-0 59375-3 0 9997
2 69613 51.8799 348.8678 0006382 247.6968 333.0366 15.37790575 2332Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-31.06923°
Longitude
101.28998°
Altitude
458.179 km
Speed
7.64 km/s
True Right ascension
13h 07m 38s
True Declination
-30° 54' 39"
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
10:22:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.47 km
Perigee altitude
448.75 km
Semi-major axis
6,831.247 km
Eccentricity
0.00064
Inclination
51.8799°
RAAN
348.8678°
Arg. of periapsis
247.6968°
True anomaly
333.00342°
Mean anomaly
333.0366°
Eccentric anomaly
333.02001°
Mean motion
3.84409 °/min
Orbital period
93.65 mins
BSTAR
0.00059375
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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-00544 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 13:44:09.271Z | 209.691° SW | 2026-06-28 13:47:09.271Z | 109.882° ESE | 36.344° | 2026-06-28 13:50:09.271Z | 61.38° ENE |
| 4 mins | 2026-06-28 15:23:09.271Z | 301.712° NW | 2026-06-28 15:24:09.271Z | 327.326° NNW | 23.035° | 2026-06-28 15:27:09.271Z | 30.451° NE |
| 5 mins | 2026-06-28 20:18:09.271Z | 324.876° NNW | 2026-06-28 20:20:09.271Z | 75.227° E | 39.062° | 2026-06-28 20:23:09.271Z | 116.622° 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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