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
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 PANDORA
1 67395U 26004AJ 26146.58518899 .00000815 00000-0 94632-4 0 9996
2 67395 97.8036 145.5803 0004920 183.0789 177.0398 14.88027288 20063Epoch: 2026-05-26T14:02Z
TLE epoch observation values (Epoch: 2026-05-26T14:02:40.328Z)
Latitude
-0.00005°
Longitude
50.75576°
Altitude
610.567 km
Speed
7.552 km/s
True Right ascension
09h 42m 19s
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
05:29:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.559 km
Perigee altitude
597.692 km
Semi-major axis
6,979.263 km
Eccentricity
0.00049
Inclination
97.8036°
RAAN
145.5803°
Arg. of periapsis
183.0789°
True anomaly
177.04271°
Mean anomaly
177.0398°
Eccentric anomaly
177.04126°
Mean motion
3.72245 °/min
Orbital period
96.71 mins
BSTAR
0.000094632
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-26 23:50:29.013Z | 161.828° S | 2026-05-26 23:54:29.013Z | 92.565° ESE | 44.377° | 2026-05-26 23:58:29.013Z | 350.595° N |
| 6 mins | 2026-05-27 13:13:29.013Z | 347.47° N | 2026-05-27 13:15:29.013Z | 290.009° WNW | 36.51° | 2026-05-27 13:19:29.013Z | 213.288° SW |
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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