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 24796U 97020E 24259.10896416 .00001202 00000-0 40442-3 0 9995
2 24796 86.3911 289.2240 0002274 88.4349 271.7108 14.36347447433005
| Epoch (UTC): | 15 September 2024 02:36:54 |
| Eccentricity: | 0.0002274 |
| inclination: | 86.3911° |
| perigee height: | 769 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 289.2240° |
| argument of perigee: | 88.4349° |
| revolutions per day: | 14.36347447 |
| mean anomaly at epoch: | 271.7108° |
| orbit number at epoch: | 43300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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