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 28308U 91082V 24357.08458380 .00002511 00000-0 10235-2 0 9990
2 28308 98.6104 23.9472 0014130 175.3069 249.6481 14.28246887 71741
| Epoch (UTC): | 22 December 2024 02:01:48 |
| Eccentricity: | 0.0014130 |
| inclination: | 98.6104° |
| perigee height: | 787 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 23.9472° |
| argument of perigee: | 175.3069° |
| revolutions per day: | 14.28246887 |
| mean anomaly at epoch: | 249.6481° |
| orbit number at epoch: | 7174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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