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: 16 hours ago
TLE from 16 hours ago
0 TPA-1
1 64533U 25135F 26132.88365606 .00002194 00000-0 10157-3 0 9996
2 64533 97.4645 248.1157 0004106 327.8717 32.2268 15.21177671 49488Epoch: 2026-05-12T21:12Z
TLE epoch observation values (Epoch: 2026-05-12T21:12:27.883Z)
Latitude
-0.00001°
Longitude
59.34788°
Altitude
502.987 km
Speed
7.614 km/s
True Right ascension
16h 32m 27s
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
22:06:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.078 km
Perigee altitude
496.43 km
Semi-major axis
6,877.391 km
Eccentricity
0.00041
Inclination
97.4645°
RAAN
248.1157°
Arg. of periapsis
327.8717°
True anomaly
32.2519°
Mean anomaly
32.2268°
Eccentric anomaly
32.23935°
Mean motion
3.80546 °/min
Orbital period
94.6 mins
BSTAR
0.00010157
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-13 19:53:27.811Z | 47.915° ENE | 2026-05-13 19:55:27.811Z | 90.788° ESE | 23.666° | 2026-05-13 19:58:27.811Z | 151.829° SSE |
| 5 mins | 2026-05-14 08:04:27.811Z | 195.266° SSW | 2026-05-14 08:06:27.811Z | 245.465° WSW | 34.578° | 2026-05-14 08:09:27.811Z | 329.98° NNW |
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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