VICTUS HAZE PUMA, 69646
Orbit data source: Space-Track
VICTUS HAZE PUMA, 69646 is a payload satellite owned by USSF SSC (US) in SSO that was launched on Fri, 19 Jun 2026 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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69646 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Operational spacecraft
Bus & Motor
PHOTON, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 VICTUS HAZE PUMA
1 69646U 26142A 26201.83709822 .00001963 00000-0 90563-4 0 9992
2 69646 97.4457 99.0756 0026523 246.3407 113.5045 15.21144501 4781Epoch: 2026-07-20T20:05Z
TLE epoch observation values (Epoch: 2026-07-20T20:05:25.286Z)
Latitude
0.00005°
Longitude
-140.89518°
Altitude
512.798 km
Speed
7.603 km/s
True Right ascension
06h 36m 18s
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
18:26:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
517.594 km
Perigee altitude
481.112 km
Semi-major axis
6,877.49 km
Eccentricity
0.00265
Inclination
97.4457°
RAAN
99.0756°
Arg. of periapsis
246.3407°
True anomaly
113.78284°
Mean anomaly
113.5045°
Eccentric anomaly
113.64371°
Mean motion
3.80538 °/min
Orbital period
94.6 mins
BSTAR
0.000090563
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Other satellites on launch #142 in the year 2026 (2026-06-19 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.VICTUS HAZE PUMA 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 | 2026-07-22 05:48:18.031Z | 22.202° NNE | 2026-07-22 05:51:18.031Z | 73.248° E | 37.878° | 2026-07-22 05:54:18.031Z | 174.013° S |
| 4 mins | 2026-07-22 16:27:18.031Z | 106.558° ESE | 2026-07-22 16:29:18.031Z | 63.805° ENE | 20.45° | 2026-07-22 16:31:18.031Z | 25.913° NE |
| 4 mins | 2026-07-22 18:01:18.031Z | 232.075° WSW | 2026-07-22 18:02:18.031Z | 253.736° W | 20.95° | 2026-07-22 18:05:18.031Z | 313.716° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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