KUIPER-00607, 69290
Orbit data source: Space-Track
KUIPER-00607, 69290 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Fri, 29 May 2026 UTC via an ATLAS V 551 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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69290 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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 KUIPER-00607
1 69290U 26118Z 26170.98998838 .00017095 00000-0 46673-3 0 9993
2 69290 51.8684 39.7153 0005968 172.5107 187.5970 15.37506633 4414Epoch: 2026-06-19T23:45Z
TLE epoch observation values (Epoch: 2026-06-19T23:45:34.996Z)
Latitude
0.00001°
Longitude
135.10845°
Altitude
458.289 km
Speed
7.637 km/s
True Right ascension
02h 38m 51s
True Declination
0° 00' 00"
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
07:12:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.03 km
Perigee altitude
449.876 km
Semi-major axis
6,832.09 km
Eccentricity
0.0006
Inclination
51.8684°
RAAN
39.7153°
Arg. of periapsis
172.5107°
True anomaly
187.58797°
Mean anomaly
187.597°
Eccentric anomaly
187.59248°
Mean motion
3.84338 °/min
Orbital period
93.67 mins
BSTAR
0.00046673
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Other satellites on launch #118 in the year 2026 (2026-05-29 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-00607 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 | 2026-06-20 23:37:51.896Z | 340.061° N | 2026-06-20 23:39:51.896Z | 36.238° NE | 26.39° | 2026-06-20 23:41:51.896Z | 82.288° E |
| 4 mins | 2026-06-21 01:15:51.896Z | 270.243° WNW | 2026-06-21 01:16:51.896Z | 238.727° WSW | 30.341° | 2026-06-21 01:19:51.896Z | 160.434° S |
| 5 mins | 2026-06-21 18:05:51.896Z | 252.155° W | 2026-06-21 18:07:51.896Z | 350.112° N | 40.648° | 2026-06-21 18:10:51.896Z | 45.996° ENE |
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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