OUT OF THE BOX, 68428
Orbit data source: Space-Track
OUT OF THE BOX, 68428 is a French payload satellite in SSO that was launched on Mon, 30 Mar 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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68428 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
Endurosat
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 OUT OF THE BOX
1 68428U 26067N 26264.32256027 .00001999 00000-0 98722-4 0 9996
2 68428 97.4686 221.6175 0002907 58.0963 302.0554 15.19031684 26536Epoch: 2026-09-21T07:44Z
TLE epoch observation values (Epoch: 2026-09-21T07:44:29.207Z)
Latitude
-0°
Longitude
105.29176°
Altitude
510.791 km
Speed
7.609 km/s
True Right ascension
14h 46m 28s
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
18:19:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.737 km
Perigee altitude
503.734 km
Semi-major axis
6,883.873 km
Eccentricity
0.00029
Inclination
97.4686°
RAAN
221.6175°
Arg. of periapsis
58.0963°
True anomaly
302.02716°
Mean anomaly
302.0554°
Eccentric anomaly
302.04128°
Mean motion
3.80009 °/min
Orbital period
94.73 mins
BSTAR
0.000098722
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.OUT OF THE BOX 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 | 2026-09-22 09:36:07.408Z | 33.526° NE | 2026-09-22 09:39:07.408Z | 92.323° ESE | 32.93° | 2026-09-22 09:42:07.408Z | 159.138° S |
| 5 mins | 2026-09-22 21:49:07.408Z | 205.647° SW | 2026-09-22 21:51:07.408Z | 253.267° W | 34.209° | 2026-09-22 21:54:07.408Z | 324.313° NNW |
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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