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 25348.25676731 .00000196 00000-0 12686-3 0 9990
2 28654 98.8294 65.4991 0013472 319.5025 40.5144 14.13682734 60185
| Epoch (UTC): | 14 December 2025 06:09:44 |
| Eccentricity: | 0.0013472 |
| inclination: | 98.8294° |
| perigee height: | 837 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 65.4991° |
| argument of perigee: | 319.5025° |
| revolutions per day: | 14.13682734 |
| mean anomaly at epoch: | 40.5144° |
| orbit number at epoch: | 6018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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