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 24298U 96051B 24282.46441699 .00000122 00000-0 92358-4 0 9993
2 24298 70.7924 189.4423 0015443 185.7675 174.3270 14.12456458448610
| Epoch (UTC): | 08 October 2024 11:08:45 |
| Eccentricity: | 0.0015443 |
| inclination: | 70.7924° |
| perigee height: | 840 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 189.4423° |
| argument of perigee: | 185.7675° |
| revolutions per day: | 14.12456458 |
| mean anomaly at epoch: | 174.3270° |
| orbit number at epoch: | 44861 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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