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 spacecraft
Bus & Motor
SATURN, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 2.0 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 PANDORA
1 67395U 26004AJ 26093.59516169 .00001853 00000-0 20804-3 0 9998
2 67395 97.8045 93.4222 0005916 29.6231 330.5320 14.87941445 12186Epoch: 2026-04-03T14:17Z
TLE epoch observation values (Epoch: 2026-04-03T14:17:01.970Z)
Latitude
0.00004°
Longitude
47.23695°
Altitude
603.807 km
Speed
7.56 km/s
True Right ascension
06h 13m 41s
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
03:53:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.523 km
Perigee altitude
597.265 km
Semi-major axis
6,979.531 km
Eccentricity
0.00059
Inclination
97.8045°
RAAN
93.4222°
Arg. of periapsis
29.6231°
True anomaly
330.49863°
Mean anomaly
330.532°
Eccentric anomaly
330.51532°
Mean motion
3.72223 °/min
Orbital period
96.72 mins
BSTAR
0.00020804
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-04 00:05:16.695Z | 174.725° S | 2026-04-04 00:08:16.695Z | 209.308° SW | 41.729° | 2026-04-04 00:12:16.695Z | 341.967° N |
| 4 mins | 2026-04-04 11:52:16.695Z | 65.504° ENE | 2026-04-04 11:54:16.695Z | 101.63° ESE | 17.97° | 2026-04-04 11:56:16.695Z | 133.203° SE |
| 6 mins | 2026-04-04 13:27:16.695Z | 342.179° N | 2026-04-04 13:29:16.695Z | 302.899° NW | 28.286° | 2026-04-04 13:33:16.695Z | 226.425° WSW |
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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