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 28654U 05018A 25347.97366071 .00000201 00000-0 12956-3 0 9998
2 28654 98.8294 65.2196 0013479 320.3544 39.6642 14.13682577 60146
| Epoch (UTC): | 13 December 2025 23:22:04 |
| Eccentricity: | 0.0013479 |
| inclination: | 98.8294° |
| perigee height: | 837 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 65.2196° |
| argument of perigee: | 320.3544° |
| revolutions per day: | 14.13682577 |
| mean anomaly at epoch: | 39.6642° |
| orbit number at epoch: | 6014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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