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, 14.5 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 PEARL-1B
1 68980U 26100A 26220.93891193 .00001151 00000-0 12276-3 0 9994
2 68980 97.7294 117.2222 0006784 345.7549 14.3477 14.90752705 14540Epoch: 2026-08-08T22:32Z
TLE epoch observation values (Epoch: 2026-08-08T22:32:01.990Z)
Latitude
-0.00004°
Longitude
-178.22916°
Altitude
594.044 km
Speed
7.565 km/s
True Right ascension
07h 48m 53s
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
21:28:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.335 km
Perigee altitude
587.877 km
Semi-major axis
6,970.743 km
Eccentricity
0.00068
Inclination
97.7294°
RAAN
117.2222°
Arg. of periapsis
345.7549°
True anomaly
14.36698°
Mean anomaly
14.3477°
Eccentric anomaly
14.35734°
Mean motion
3.72928 °/min
Orbital period
96.53 mins
BSTAR
0.00012276
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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 | 2026-08-09 16:23:53.472Z | 120.338° SE | 2026-08-09 16:26:53.472Z | 65.28° ENE | 23.552° | 2026-08-09 16:29:53.472Z | 15.476° NNE |
| 4 mins | 2026-08-09 18:00:53.472Z | 235.013° WSW | 2026-08-09 18:01:53.472Z | 255.596° W | 21.881° | 2026-08-09 18:04:53.472Z | 311.884° NW |
| 6 mins | 2026-08-10 05:43:53.472Z | 33.046° NE | 2026-08-10 05:45:53.472Z | 85.879° E | 38.116° | 2026-08-10 05:49:53.472Z | 176.057° S |
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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