KUIPER-00101, 65947
Orbit data source: Space-Track
KUIPER-00101, 65947 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Tue, 14 Oct 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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65947 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00101
1 65947U 25228A 26170.53034199 .00002593 00000-0 36903-3 0 9993
2 65947 51.8981 270.2212 0000594 105.1511 254.9517 14.79932595 38315Epoch: 2026-06-19T12:43Z
TLE epoch observation values (Epoch: 2026-06-19T12:43:41.547Z)
Latitude
-0.00005°
Longitude
171.54006°
Altitude
630.392 km
Speed
7.544 km/s
True Right ascension
18h 00m 53s
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
07:14:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.405 km
Perigee altitude
629.572 km
Semi-major axis
7,008.125 km
Eccentricity
0.00006
Inclination
51.8981°
RAAN
270.2212°
Arg. of periapsis
105.1511°
True anomaly
254.94513°
Mean anomaly
254.9517°
Eccentric anomaly
254.94841°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00036903
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Other satellites on launch #228 in the year 2025 (2025-10-14 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-00101 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 08:39:06.154Z | 209.838° SW | 2026-06-21 08:43:06.154Z | 116.694° SE | 37.878° | 2026-06-21 08:47:06.154Z | 60.596° ENE |
| 6 mins | 2026-06-21 10:22:06.154Z | 285.137° WNW | 2026-06-21 10:24:06.154Z | 327.313° NNW | 29.16° | 2026-06-21 10:28:06.154Z | 37.896° NE |
| 4 mins | 2026-06-21 12:05:06.154Z | 327.108° NNW | 2026-06-21 12:07:06.154Z | 359.153° N | 17.401° | 2026-06-21 12:09:06.154Z | 29.443° NE |
| 6 mins | 2026-06-21 13:47:06.154Z | 334.063° NNW | 2026-06-21 13:50:06.154Z | 27.103° NE | 21.844° | 2026-06-21 13:53:06.154Z | 70.072° E |
| 7 mins | 2026-06-21 15:29:06.154Z | 312.831° NW | 2026-06-21 15:32:06.154Z | 92.095° ESE | 43.263° | 2026-06-21 15:36:06.154Z | 123.768° SE |
| 4 mins | 2026-06-21 17:11:06.154Z | 257.243° W | 2026-06-21 17:13:06.154Z | 225.53° WSW | 16.458° | 2026-06-21 17:15:06.154Z | 197.265° SSW |
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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