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 23085.81617948 .00009494 00000-0 87879-3 0 9991
2 40024 98.0206 38.9926 0010503 183.5534 176.5613 14.94701986476108
| Epoch (UTC): | 26 March 2023 19:35:17 |
| Eccentricity: | 0.0010503 |
| inclination: | 98.0206° |
| perigee height: | 576 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 38.9926° |
| argument of perigee: | 183.5534° |
| revolutions per day: | 14.94701986 |
| mean anomaly at epoch: | 176.5613° |
| orbit number at epoch: | 47610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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