OBJECT L, 68426
Orbit data source: Space-Track
OBJECT L, 68426 is a 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). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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68426 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
Endurosat
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT L
1 68426U 26067L 26262.12931605 .00011314 00000-0 50461-3 0 9991
2 68426 97.4641 219.7284 0003125 61.0749 299.0800 15.21561554 26225Epoch: 2026-09-19T03:06Z
TLE epoch observation values (Epoch: 2026-09-19T03:06:12.906Z)
Latitude
-0.00003°
Longitude
175.13235°
Altitude
503.176 km
Speed
7.613 km/s
True Right ascension
14h 38m 54s
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
09:41:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.245 km
Perigee altitude
495.947 km
Semi-major axis
6,876.233 km
Eccentricity
0.00031
Inclination
97.4641°
RAAN
219.7284°
Arg. of periapsis
61.0749°
True anomaly
299.0487°
Mean anomaly
299.08°
Eccentric anomaly
299.06435°
Mean motion
3.80643 °/min
Orbital period
94.58 mins
BSTAR
0.00050461
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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.OBJECT L 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-20 20:18:00.551Z | 99.377° ESE | 2026-09-20 20:20:00.551Z | 64.863° ENE | 14.826° | 2026-09-20 20:22:00.551Z | 31.798° NE |
| 4 mins | 2026-09-20 21:52:00.551Z | 221.083° SW | 2026-09-20 21:53:00.551Z | 249.742° W | 32.575° | 2026-09-20 21:56:00.551Z | 322.794° NNW |
| 4 mins | 2026-09-21 10:55:00.551Z | 328.716° NNW | 2026-09-21 10:57:00.551Z | 282.963° WNW | 23.41° | 2026-09-21 10:59:00.551Z | 243.419° 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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