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 24251.21489406 .00029034 00000-0 19881-2 0 9996
2 40024 98.0712 226.8942 0003648 234.2638 125.8248 15.06025538556103
| Epoch (UTC): | 07 September 2024 05:09:26 |
| Eccentricity: | 0.0003648 |
| inclination: | 98.0712° |
| perigee height: | 546 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 226.8942° |
| argument of perigee: | 234.2638° |
| revolutions per day: | 15.06025538 |
| mean anomaly at epoch: | 125.8248° |
| orbit number at epoch: | 55610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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