KUIPER-00546, 69614
Orbit data source: Space-Track
KUIPER-00546, 69614 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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69614 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-00546
1 69614U 26140Y 26178.50002315 .00026301 00000-0 68748-3 0 9997
2 69614 51.8791 348.7115 0015425 196.5710 101.5973 15.38470705 2765Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-44.01157°
Longitude
-155.83745°
Altitude
467.446 km
Speed
7.631 km/s
True Right ascension
19h 59m 08s
True Declination
-43° 49' 57"
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
10:52:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.631 km
Perigee altitude
440.563 km
Semi-major axis
6,829.234 km
Eccentricity
0.00154
Inclination
51.8791°
RAAN
348.7115°
Arg. of periapsis
196.571°
True anomaly
101.77038°
Mean anomaly
101.5973°
Eccentric anomaly
101.68385°
Mean motion
3.84579 °/min
Orbital period
93.61 mins
BSTAR
0.00068748
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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-00546 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 13:22:04.957Z | 197.54° SSW | 2026-06-28 13:25:04.957Z | 137.946° SSE | 27.693° | 2026-06-28 13:28:04.957Z | 72.65° E |
| 4 mins | 2026-06-28 15:01:04.957Z | 283.784° WNW | 2026-06-28 15:03:04.957Z | 348.33° N | 28.25° | 2026-06-28 15:05:04.957Z | 30.938° NE |
| 5 mins | 2026-06-28 19:56:04.957Z | 334.183° NNW | 2026-06-28 19:58:04.957Z | 43.869° NE | 32.573° | 2026-06-28 20:01:04.957Z | 102.678° 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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