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 28096U 03054B 25322.04173479 -.00000002 00000-0 15055-3 0 9998
2 28096 63.6784 208.1782 0078926 129.6494 231.1531 13.41051092 74100
| Epoch (UTC): | 18 November 2025 01:00:05 |
| Eccentricity: | 0.0078926 |
| inclination: | 63.6784° |
| perigee height: | 1046 km |
| apogee height: | 1164 km |
| right ascension of ascending node: | 208.1782° |
| argument of perigee: | 129.6494° |
| revolutions per day: | 13.41051092 |
| mean anomaly at epoch: | 231.1531° |
| orbit number at epoch: | 7410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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