KUIPER-00557, 69622
Orbit data source: Space-Track
KUIPER-00557, 69622 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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69622 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: 5 hours ago
TLE from 5 hours ago
0 KUIPER-00557
1 69622U 26140AG 26178.91668981 .00064116 00000-0 16407-2 0 9998
2 69622 51.8813 346.7773 0010420 227.2396 180.9137 15.38761939 1718Epoch: 2026-06-27T22:00Z
TLE epoch observation values (Epoch: 2026-06-27T22:00:01.999Z)
Latitude
35.99623°
Longitude
135.27432°
Altitude
459.515 km
Speed
7.638 km/s
True Right ascension
01h 25m 13s
True Declination
35° 49' 33"
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
14:19:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.35 km
Perigee altitude
443.12 km
Semi-major axis
6,828.372 km
Eccentricity
0.00104
Inclination
51.8813°
RAAN
346.7773°
Arg. of periapsis
227.2396°
True anomaly
180.9118°
Mean anomaly
180.9137°
Eccentric anomaly
180.91275°
Mean motion
3.84651 °/min
Orbital period
93.59 mins
BSTAR
0.0016407
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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-00557 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 13:32:12.088Z | 205.916° SW | 2026-06-28 13:35:12.088Z | 151.213° SSE | 31.838° | 2026-06-28 13:38:12.088Z | 70.194° E |
| 4 mins | 2026-06-28 15:11:12.088Z | 284.854° WNW | 2026-06-28 15:13:12.088Z | 337.903° N | 25.953° | 2026-06-28 15:15:12.088Z | 25.149° NE |
| 5 mins | 2026-06-28 20:06:12.088Z | 326.684° NNW | 2026-06-28 20:08:12.088Z | 35.206° NE | 36.934° | 2026-06-28 20:11:12.088Z | 107.638° 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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