KUIPER-00547, 69615
Orbit data source: Space-Track
KUIPER-00547, 69615 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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69615 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-00547
1 69615U 26140Z 26178.50002315 .00025861 00000-0 66372-3 0 9999
2 69615 51.8827 348.7744 0011622 215.9451 52.4954 15.39094071 1308Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-52.01378°
Longitude
160.80385°
Altitude
461.862 km
Speed
7.638 km/s
True Right ascension
17h 05m 42s
True Declination
-51° 50' 23"
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
09:21:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.187 km
Perigee altitude
441.318 km
Semi-major axis
6,827.39 km
Eccentricity
0.00116
Inclination
51.8827°
RAAN
348.7744°
Arg. of periapsis
215.9451°
True anomaly
52.60114°
Mean anomaly
52.4954°
Eccentric anomaly
52.54826°
Mean motion
3.84735 °/min
Orbital period
93.57 mins
BSTAR
0.00066372
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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-00547 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-28 13:31:04.705Z | 183.352° SSW | 2026-06-28 13:32:04.705Z | 154.285° SSE | 30.007° | 2026-06-28 13:35:04.705Z | 72.532° E |
| 5 mins | 2026-06-28 15:08:04.705Z | 282.058° WNW | 2026-06-28 15:10:04.705Z | 335.135° NNW | 26.827° | 2026-06-28 15:13:04.705Z | 35.33° NE |
| 5 mins | 2026-06-28 20:03:04.705Z | 327.907° NNW | 2026-06-28 20:05:04.705Z | 33.459° NE | 35.702° | 2026-06-28 20:08:04.705Z | 105.59° 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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