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 26317.71874762 .00002564 00000-0 26432-3 0 9998
2 68980 97.7191 211.9227 0007801 23.3295 336.8276 14.91072086 28969Epoch: 2026-11-13T17:14Z
TLE epoch observation values (Epoch: 2026-11-13T17:14:59.794Z)
Latitude
-0.00002°
Longitude
-99.6603°
Altitude
592.632 km
Speed
7.566 km/s
True Right ascension
14h 07m 41s
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
21:09:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.047 km
Perigee altitude
586.172 km
Semi-major axis
6,969.746 km
Eccentricity
0.00078
Inclination
97.7191°
RAAN
211.9227°
Arg. of periapsis
23.3295°
True anomaly
336.79239°
Mean anomaly
336.8276°
Eccentric anomaly
336.81°
Mean motion
3.73008 °/min
Orbital period
96.51 mins
BSTAR
0.00026432
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-14 05:06:20.833Z | 46.322° ENE | 2026-11-14 05:09:20.833Z | 95.468° ESE | 21.701° | 2026-11-14 05:12:20.833Z | 143.621° SSE |
| 6 mins | 2026-11-14 06:42:20.833Z | 340.526° N | 2026-11-14 06:45:20.833Z | 277.813° WNW | 28.633° | 2026-11-14 06:48:20.833Z | 230.974° WSW |
| 6 mins | 2026-11-14 17:32:20.833Z | 194.686° SSW | 2026-11-14 17:35:20.833Z | 275.404° WNW | 44.744° | 2026-11-14 17:38:20.833Z | 331.492° NNW |
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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