KUIPER-00083, 64829
Orbit data source: Space-Track
KUIPER-00083, 64829 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Wed, 16 Jul 2025 UTC via an FALCON 9 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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64829 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 KUIPER-00083
1 64829U 25151P 26166.41360913 .00000295 00000-0 67755-4 0 9991
2 64829 51.8997 223.4642 0000486 100.8463 259.2555 14.79931577 51038Epoch: 2026-06-15T09:55Z
TLE epoch observation values (Epoch: 2026-06-15T09:55:35.828Z)
Latitude
0.00004°
Longitude
170.8646°
Altitude
630.35 km
Speed
7.544 km/s
True Right ascension
14h 53m 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
14:42:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.332 km
Perigee altitude
629.651 km
Semi-major axis
7,008.128 km
Eccentricity
0.00005
Inclination
51.8997°
RAAN
223.4642°
Arg. of periapsis
100.8463°
True anomaly
259.25003°
Mean anomaly
259.2555°
Eccentric anomaly
259.25276°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.000067755
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Other satellites on launch #151 in the year 2025 (2025-07-16 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-00083 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-16 05:30:50.406Z | 186.604° SSW | 2026-06-16 05:34:50.406Z | 124.894° SE | 23.646° | 2026-06-16 05:37:50.406Z | 78.514° E |
| 7 mins | 2026-06-16 07:12:50.406Z | 254.473° W | 2026-06-16 07:15:50.406Z | 328.732° NNW | 39.59° | 2026-06-16 07:19:50.406Z | 44.644° NE |
| 5 mins | 2026-06-16 08:55:50.406Z | 310.655° NW | 2026-06-16 08:57:50.406Z | 343.06° N | 19.646° | 2026-06-16 09:00:50.406Z | 30.298° NE |
| 5 mins | 2026-06-16 10:38:50.406Z | 336.817° NNW | 2026-06-16 10:40:50.406Z | 9.088° NNE | 18.449° | 2026-06-16 10:43:50.406Z | 52.976° ENE |
| 6 mins | 2026-06-16 12:20:50.406Z | 329.906° NNW | 2026-06-16 12:22:50.406Z | 14.226° NNE | 34.395° | 2026-06-16 12:26:50.406Z | 99.206° ESE |
| 6 mins | 2026-06-16 14:01:50.406Z | 282.723° WNW | 2026-06-16 14:04:50.406Z | 220.729° SW | 29.805° | 2026-06-16 14:07:50.406Z | 167.53° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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