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 40024U 14033Q 24340.50947437 .00022088 00000-0 13379-2 0 9998
2 40024 98.0812 320.7444 0004474 338.9327 21.1716 15.10602887569048
| Epoch (UTC): | 05 December 2024 12:13:38 |
| Eccentricity: | 0.0004474 |
| inclination: | 98.0812° |
| perigee height: | 531 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 320.7444° |
| argument of perigee: | 338.9327° |
| revolutions per day: | 15.10602887 |
| mean anomaly at epoch: | 21.1716° |
| orbit number at epoch: | 56904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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