KUIPER-00248, 67153
Orbit data source: Space-Track
KUIPER-00248, 67153 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 15 Dec 2025 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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67153 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: 13 hours ago
TLE from 13 hours ago
0 KUIPER-00248
1 67153U 25301W 26171.37690309 .00001778 00000-0 28248-3 0 9997
2 67153 51.8994 306.4082 0001755 71.5018 288.6134 14.76642521 29453Epoch: 2026-06-20T09:02Z
TLE epoch observation values (Epoch: 2026-06-20T09:02:44.426Z)
Latitude
-0.00001°
Longitude
-97.86932°
Altitude
640.295 km
Speed
7.539 km/s
True Right ascension
20h 25m 37s
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
08:32:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.624 km
Perigee altitude
639.161 km
Semi-major axis
7,018.53 km
Eccentricity
0.00018
Inclination
51.8994°
RAAN
306.4082°
Arg. of periapsis
71.5018°
True anomaly
288.59434°
Mean anomaly
288.6134°
Eccentric anomaly
288.60387°
Mean motion
3.69125 °/min
Orbital period
97.53 mins
BSTAR
0.00028248
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Other satellites on launch #301 in the year 2025 (2025-12-15 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-00248 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 11:11:01.740Z | 209.739° SW | 2026-06-21 11:15:01.740Z | 153.112° SSE | 36.345° | 2026-06-21 11:19:01.740Z | 65.027° ENE |
| 7 mins | 2026-06-21 12:54:01.740Z | 272.908° WNW | 2026-06-21 12:57:01.740Z | 327.22° NNW | 30.495° | 2026-06-21 13:01:01.740Z | 38.464° NE |
| 5 mins | 2026-06-21 14:38:01.740Z | 323.793° NNW | 2026-06-21 14:40:01.740Z | 355.266° N | 17.846° | 2026-06-21 14:43:01.740Z | 37.735° NE |
| 5 mins | 2026-06-21 16:21:01.740Z | 341.302° N | 2026-06-21 16:23:01.740Z | 17.407° NNE | 21.911° | 2026-06-21 16:26:01.740Z | 64.648° ENE |
| 7 mins | 2026-06-21 18:02:01.740Z | 312.711° NW | 2026-06-21 18:05:01.740Z | 2.573° NNE | 43.423° | 2026-06-21 18:09:01.740Z | 120.448° SE |
| 4 mins | 2026-06-21 19:45:01.740Z | 257.26° W | 2026-06-21 19:47:01.740Z | 224.253° SW | 17.769° | 2026-06-21 19:49:01.740Z | 195.317° 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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