OBJECT E, 68984
Orbit data source: Space-Track
OBJECT E, 68984 is a satellite in SSO that was launched on Sun, 03 May 2026 UTC launched 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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68984 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
Unknown
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT E
1 68984U 26100E 26130.16668980 .00050082 00000-0 50313-2 0 9999
2 68984 97.7370 28.3212 0002712 284.6670 17.8888 14.91047362 1551Epoch: 2026-05-10T04:00Z
TLE epoch observation values (Epoch: 2026-05-10T04:00:01.998Z)
Latitude
-56.85582°
Longitude
112.28185°
Altitude
614.92 km
Speed
7.551 km/s
True Right ascension
02h 41m 03s
True Declination
-56° 41' 42"
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
18:58:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.578 km
Perigee altitude
589.797 km
Semi-major axis
6,969.824 km
Eccentricity
0.00027
Inclination
97.737°
RAAN
28.3212°
Arg. of periapsis
284.667°
True anomaly
17.89835°
Mean anomaly
17.8888°
Eccentric anomaly
17.89357°
Mean motion
3.73001 °/min
Orbital period
96.51 mins
BSTAR
0.0050313
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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 E 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 | 2026-05-10 17:15:39.781Z | 169.761° S | 2026-05-10 17:19:39.781Z | 320.881° NNW | 43.752° | 2026-05-10 17:22:39.781Z | 345.192° N |
| 5 mins | 2026-05-11 06:36:39.781Z | 340.154° N | 2026-05-11 06:38:39.781Z | 287.057° WNW | 32.033° | 2026-05-11 06:41:39.781Z | 224.805° 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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