KUIPER-00549, 69616
Orbit data source: Space-Track
KUIPER-00549, 69616 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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69616 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-00549
1 69616U 26140AA 26178.50002315 .00020574 00000-0 56958-3 0 9995
2 69616 51.8804 348.9276 0006144 311.9119 239.2135 15.36941610 2671Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-8.81288°
Longitude
80.25448°
Altitude
459.636 km
Speed
7.636 km/s
True Right ascension
11h 43m 30s
True Declination
-8° 45' 31"
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
10:51:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.824 km
Perigee altitude
451.426 km
Semi-major axis
6,833.762 km
Eccentricity
0.00061
Inclination
51.8804°
RAAN
348.9276°
Arg. of periapsis
311.9119°
True anomaly
239.15304°
Mean anomaly
239.2135°
Eccentric anomaly
239.18327°
Mean motion
3.84196 °/min
Orbital period
93.7 mins
BSTAR
0.00056958
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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-00549 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 13:52:45.807Z | 218.114° SW | 2026-06-28 13:55:45.807Z | 121.31° SE | 41.301° | 2026-06-28 13:58:45.807Z | 58.876° ENE |
| 4 mins | 2026-06-28 15:31:45.807Z | 298.281° NW | 2026-06-28 15:33:45.807Z | 345.936° N | 21.022° | 2026-06-28 15:35:45.807Z | 25.161° NE |
| 5 mins | 2026-06-28 20:26:45.807Z | 314.515° NW | 2026-06-28 20:28:45.807Z | 28.74° NE | 43.852° | 2026-06-28 20:31:45.807Z | 121.424° 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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