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 spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OUT OF THE BOX
1 68428U 26067N 26171.41668980 -.00003947 00000-0 -18815-3 0 9999
2 68428 97.4580 129.8870 0002111 42.8076 266.0261 15.18536342 1305Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-50.84683°
Longitude
80.44775°
Altitude
530.15 km
Speed
7.596 km/s
True Right ascension
09h 16m 21s
True Declination
-50° 40' 22"
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
15:16:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.687 km
Perigee altitude
505.78 km
Semi-major axis
6,885.37 km
Eccentricity
0.00021
Inclination
97.458°
RAAN
129.887°
Arg. of periapsis
42.8076°
True anomaly
266.00197°
Mean anomaly
266.0261°
Eccentric anomaly
266.01403°
Mean motion
3.79885 °/min
Orbital period
94.77 mins
BSTAR
-0.00018815
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:13:20.736Z | 8.056° NNE | 2026-06-22 10:17:20.736Z | 230.562° WSW | 42.12° | 2026-06-22 10:20:20.736Z | 199.209° SSW |
| 5 mins | 2026-06-22 20:53:20.736Z | 132.112° SE | 2026-06-22 20:55:20.736Z | 74.446° E | 33.127° | 2026-06-22 20:58:20.736Z | 5.985° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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