KUIPER-00537, 69607
Orbit data source: Space-Track
KUIPER-00537, 69607 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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69607 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: 13 hours ago
TLE from 13 hours ago
0 KUIPER-00537
1 69607U 26140R 26178.50002315 .00031386 00000-0 89504-3 0 9991
2 69607 51.8822 349.0066 0008266 350.7081 164.3923 15.35756919 2494Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
19.36619°
Longitude
57.46739°
Altitude
464.399 km
Speed
7.634 km/s
True Right ascension
10h 12m 21s
True Declination
19° 15' 15"
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
12:37:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.79 km
Perigee altitude
453.487 km
Semi-major axis
6,837.275 km
Eccentricity
0.00083
Inclination
51.8822°
RAAN
349.0066°
Arg. of periapsis
350.7081°
True anomaly
164.41776°
Mean anomaly
164.3923°
Eccentric anomaly
164.40503°
Mean motion
3.839 °/min
Orbital period
93.77 mins
BSTAR
0.00089504
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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-00537 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 14:03:10.442Z | 227.235° WSW | 2026-06-28 14:06:10.442Z | 206.052° SW | 42.631° | 2026-06-28 14:09:10.442Z | 55.153° ENE |
| 4 mins | 2026-06-28 15:43:10.442Z | 307.57° NW | 2026-06-28 15:44:10.442Z | 329.124° NNW | 18.979° | 2026-06-28 15:47:10.442Z | 27.768° NE |
| 5 mins | 2026-06-28 20:38:10.442Z | 306.966° NW | 2026-06-28 20:40:10.442Z | 154.847° SSE | 44.892° | 2026-06-28 20:43:10.442Z | 129.715° 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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