BUSANSAT, 68989
Orbit data source: Space-Track
BUSANSAT, 68989 is a South Korean payload 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). 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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68989 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 BUSANSAT
1 68989U 26100K 26265.94742482 .00001099 00000-0 11621-3 0 9993
2 68989 97.7254 161.3842 0006317 157.6585 202.4910 14.91158912 21265Epoch: 2026-09-22T22:44Z
TLE epoch observation values (Epoch: 2026-09-22T22:44:17.504Z)
Latitude
-0°
Longitude
178.50568°
Altitude
601.433 km
Speed
7.557 km/s
True Right ascension
10h 45m 32s
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
04:08:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.742 km
Perigee altitude
586.936 km
Semi-major axis
6,969.476 km
Eccentricity
0.00063
Inclination
97.7254°
RAAN
161.3842°
Arg. of periapsis
157.6585°
True anomaly
202.46333°
Mean anomaly
202.491°
Eccentric anomaly
202.47716°
Mean motion
3.73029 °/min
Orbital period
96.51 mins
BSTAR
0.00011621
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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.BUSANSAT 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-23 16:35:27.689Z | 131.941° SE | 2026-09-23 16:38:27.689Z | 71.953° E | 35.494° | 2026-09-23 16:41:27.689Z | 11.353° NNE |
| 4 mins | 2026-09-23 18:12:27.689Z | 237.577° WSW | 2026-09-23 18:14:27.689Z | 272.01° WNW | 17.714° | 2026-09-23 18:16:27.689Z | 303.492° NW |
| 6 mins | 2026-09-24 05:55:27.689Z | 19.895° NNE | 2026-09-24 05:57:27.689Z | 58.765° ENE | 69.844° | 2026-09-24 06:01:27.689Z | 187.107° SSW |
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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