PEARL-1B, 68980
Orbit data source: Space-Track
PEARL-1B, 68980 is a Taiwanese 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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68980 intel report (Beta)
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Identifier
Orbit
Country
TW / TWNRelated business
Manufacturer
Endurosat
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6UXL, Unknown motor
Mass
8.8 kg wet, 8.8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 PEARL-1B
1 68980U 26100A 26266.17691904 .00001328 00000-0 14022-3 0 9995
2 68980 97.7227 161.4973 0007112 170.1495 189.9864 14.90885895 21281Epoch: 2026-09-23T04:14Z
TLE epoch observation values (Epoch: 2026-09-23T04:14:45.805Z)
Latitude
-0.00001°
Longitude
95.77465°
Altitude
603.099 km
Speed
7.555 km/s
True Right ascension
10h 45m 59s
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
04:08:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.148 km
Perigee altitude
587.233 km
Semi-major axis
6,970.327 km
Eccentricity
0.00071
Inclination
97.7227°
RAAN
161.4973°
Arg. of periapsis
170.1495°
True anomaly
189.97228°
Mean anomaly
189.9864°
Eccentric anomaly
189.97934°
Mean motion
3.72961 °/min
Orbital period
96.52 mins
BSTAR
0.00014022
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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.PEARL-1B 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-23 17:14:50.914Z | 172.123° S | 2026-09-23 17:18:50.914Z | 289.323° WNW | 74.323° | 2026-09-23 17:22:50.914Z | 344.58° N |
| 4 mins | 2026-09-24 05:00:50.914Z | 66.661° ENE | 2026-09-24 05:02:50.914Z | 101.468° ESE | 17.14° | 2026-09-24 05:04:50.914Z | 131.817° SE |
| 6 mins | 2026-09-24 06:35:50.914Z | 341.846° N | 2026-09-24 06:37:50.914Z | 297.638° NW | 35.284° | 2026-09-24 06:41:50.914Z | 222.732° SW |
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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