View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 01002U 65008C 25347.05501076 -.00000002 00000-0 -13608-2 0 9991
2 01002 32.1395 125.6425 0015792 319.3444 40.5874 9.88354972197779
| Epoch (UTC): | 13 December 2025 01:19:12 |
| Eccentricity: | 0.0015792 |
| inclination: | 32.1395° |
| perigee height: | 2779 km |
| apogee height: | 2808 km |
| right ascension of ascending node: | 125.6425° |
| argument of perigee: | 319.3444° |
| revolutions per day: | 9.88354972 |
| mean anomaly at epoch: | 40.5874° |
| orbit number at epoch: | 19777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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