OBJECT A, 69502
Orbit data source: Space-Track
OBJECT A, 69502 is a satellite in SSO that was launched on Fri, 12 Jun 2026 UTC via a H3-30S launch vehicle from the Tanegashima Space Center (TNSTA). 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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69502 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT A
1 69502U 26132A 26164.48383071 .00000623 00000-0 56191-4 0 9996
2 69502 97.6918 228.2077 0012143 285.1464 74.8416 14.99040716 228Epoch: 2026-06-13T11:36Z
TLE epoch observation values (Epoch: 2026-06-13T11:36:42.973Z)
Latitude
0.00003°
Longitude
152.23037°
Altitude
570.715 km
Speed
7.577 km/s
True Right ascension
15h 12m 49s
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
05:02:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.298 km
Perigee altitude
558.432 km
Semi-major axis
6,945.002 km
Eccentricity
0.00121
Inclination
97.6918°
RAAN
228.2077°
Arg. of periapsis
285.1464°
True anomaly
74.97596°
Mean anomaly
74.8416°
Eccentric anomaly
74.90877°
Mean motion
3.75003 °/min
Orbital period
96 mins
BSTAR
0.000056191
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Other satellites on launch #132 in the year 2026 (2026-06-12 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 A 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 | 2026-06-14 03:45:23.210Z | 139.483° SSE | 2026-06-14 03:49:23.210Z | 61.426° ENE | 30.928° | 2026-06-14 03:52:23.210Z | 7.313° NNE |
| 6 mins | 2026-06-14 17:01:23.210Z | 18.681° NNE | 2026-06-14 17:04:23.210Z | 114.94° SE | 43.632° | 2026-06-14 17:07:23.210Z | 185.108° SSW |
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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