PANDORA, 67395
Orbit data source: Space-Track
PANDORA, 67395 is a payload satellite owned by GSFC (US) in SSO that was launched on Sun, 11 Jan 2026 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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67395 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
BLCAN/LLNL
Mission
Operational Civil Astronomy
Bus & Motor
SATURN, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + Cyl + 1 Pan, 2.0 m
Radar Cross Section
2.532 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 PANDORA
1 67395U 26004AJ 26206.63208365 .00000878 00000-0 10125-3 0 9996
2 67395 97.8057 204.6962 0005614 19.3924 340.7505 14.88134422 28990Epoch: 2026-07-25T15:10Z
TLE epoch observation values (Epoch: 2026-07-25T15:10:12.027Z)
Latitude
-0.00004°
Longitude
33.80451°
Altitude
603.099 km
Speed
7.56 km/s
True Right ascension
13h 38m 47s
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
10:26:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.709 km
Perigee altitude
596.873 km
Semi-major axis
6,978.928 km
Eccentricity
0.00056
Inclination
97.8057°
RAAN
204.6962°
Arg. of periapsis
19.3924°
True anomaly
340.72928°
Mean anomaly
340.7505°
Eccentric anomaly
340.73989°
Mean motion
3.72272 °/min
Orbital period
96.7 mins
BSTAR
0.00010125
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Other satellites on launch #4 in the year 2026 (2026-01-11 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.PANDORA 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 | 2026-07-25 23:22:42.473Z | 131.285° SE | 2026-07-25 23:25:42.473Z | 68.257° E | 30.32° | 2026-07-25 23:28:42.473Z | 10.151° NNE |
| 4 mins | 2026-07-26 00:59:42.473Z | 236.55° WSW | 2026-07-26 01:01:42.473Z | 270.408° WNW | 16.763° | 2026-07-26 01:03:42.473Z | 302.201° NW |
| 6 mins | 2026-07-26 12:43:42.473Z | 17.506° NNE | 2026-07-26 12:46:42.473Z | 139.277° SSE | 43.984° | 2026-07-26 12:49:42.473Z | 187.639° SSW |
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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