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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 TPA-1
1 64533U 25135F 26178.26710457 .00004299 00000-0 19367-3 0 9996
2 64533 97.4696 293.1272 0006045 142.9577 217.2077 15.21574484 56389Epoch: 2026-06-27T06:24Z
TLE epoch observation values (Epoch: 2026-06-27T06:24:37.834Z)
Latitude
-0.00006°
Longitude
-78.41415°
Altitude
507.495 km
Speed
7.608 km/s
True Right ascension
19h 32m 30s
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
05:12:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.214 km
Perigee altitude
493.901 km
Semi-major axis
6,876.194 km
Eccentricity
0.0006
Inclination
97.4696°
RAAN
293.1272°
Arg. of periapsis
142.9577°
True anomaly
217.16584°
Mean anomaly
217.2077°
Eccentric anomaly
217.18677°
Mean motion
3.80646 °/min
Orbital period
94.58 mins
BSTAR
0.00019367
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-27 21:11:52.194Z | 323.808° NNW | 2026-06-27 21:12:52.194Z | 296.773° NW | 25.463° | 2026-06-27 21:15:52.194Z | 231.396° WSW |
| 6 mins | 2026-06-28 07:47:52.194Z | 172.2° S | 2026-06-28 07:49:52.194Z | 190.187° SSW | 41.996° | 2026-06-28 07:53:52.194Z | 345.511° 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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