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 24284.31722981 .00000040 00000-0 22313-3 0 9998
2 28096 63.6779 147.4031 0108459 162.2106 198.2765 13.40995641 19965
| Epoch (UTC): | 10 October 2024 07:36:48 |
| Eccentricity: | 0.0108459 |
| inclination: | 63.6779° |
| perigee height: | 1024 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 147.4031° |
| argument of perigee: | 162.2106° |
| revolutions per day: | 13.40995641 |
| mean anomaly at epoch: | 198.2765° |
| orbit number at epoch: | 1996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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