OBJECT K, 68989
Orbit data source: Space-Track
OBJECT K, 68989 is a satellite in SSO that was launched on Sun, 03 May 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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68989 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown shape, 1.1 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 OBJECT K
1 68989U 26100K 26174.27647232 .00001559 00000-0 16370-3 0 9992
2 68989 97.7389 71.5627 0007551 109.8645 250.3388 14.90885594 7609Epoch: 2026-06-23T06:38Z
TLE epoch observation values (Epoch: 2026-06-23T06:38:07.208Z)
Latitude
0.00001°
Longitude
60.58231°
Altitude
599.989 km
Speed
7.559 km/s
True Right ascension
04h 46m 15s
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
07:37:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.455 km
Perigee altitude
586.929 km
Semi-major axis
6,970.329 km
Eccentricity
0.00076
Inclination
97.7389°
RAAN
71.5627°
Arg. of periapsis
109.8645°
True anomaly
250.25734°
Mean anomaly
250.3388°
Eccentric anomaly
250.29807°
Mean motion
3.72961 °/min
Orbital period
96.52 mins
BSTAR
0.0001637
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Other satellites on launch #100 in the year 2026 (2026-05-03 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 K 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 | 2026-06-25 05:55:05.524Z | 18.402° NNE | 2026-06-25 05:58:05.524Z | 67.885° E | 42.849° | 2026-06-25 06:02:05.524Z | 185.683° SSW |
| 6 mins | 2026-06-25 16:46:05.524Z | 134.61° SE | 2026-06-25 16:48:05.524Z | 91.695° ESE | 33.649° | 2026-06-25 16:52:05.524Z | 3.227° 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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