TPA-1, 64533
Orbit data source: Space-Track
TPA-1, 64533 is a New Zealander payload satellite in SSO that was launched on Mon, 23 Jun 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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64533 intel report (Beta)
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Identifier
Orbit
Country
NZRelated business
Manufacturer
NANAV/TPA
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.5 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 TPA-1
1 64533U 25135F 26104.85942075 .00002227 00000-0 10358-3 0 9993
2 64533 97.4603 220.3480 0006466 60.9821 299.2062 15.20987778 45226Epoch: 2026-04-14T20:37Z
TLE epoch observation values (Epoch: 2026-04-14T20:37:33.952Z)
Latitude
-0.00002°
Longitude
67.92691°
Altitude
503.781 km
Speed
7.614 km/s
True Right ascension
14h 41m 23s
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
20:21:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.274 km
Perigee altitude
495.379 km
Semi-major axis
6,877.964 km
Eccentricity
0.00065
Inclination
97.4603°
RAAN
220.348°
Arg. of periapsis
60.9821°
True anomaly
299.1415°
Mean anomaly
299.2062°
Eccentric anomaly
299.17385°
Mean motion
3.80499 °/min
Orbital period
94.61 mins
BSTAR
0.00010358
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Other satellites on launch #135 in the year 2025 (2025-06-23 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.TPA-1 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 | 2026-04-15 20:52:25.078Z | 354.92° N | 2026-04-15 20:55:25.078Z | 264.804° W | 35.205° | 2026-04-15 20:58:25.078Z | 212.295° SW |
| 5 mins | 2026-04-16 07:30:25.078Z | 148.951° SSE | 2026-04-16 07:32:25.078Z | 79.597° E | 41.091° | 2026-04-16 07:35:25.078Z | 357.303° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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