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 25137.20996290 -.00000175 00000-0 -68310-4 0 9998
2 24298 70.7696 82.6803 0017276 219.3646 140.6219 14.12422534480040
| Epoch (UTC): | 17 May 2025 05:02:20 |
| Eccentricity: | 0.0017276 |
| inclination: | 70.7696° |
| perigee height: | 838 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 82.6803° |
| argument of perigee: | 219.3646° |
| revolutions per day: | 14.12422534 |
| mean anomaly at epoch: | 140.6219° |
| orbit number at epoch: | 48004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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