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 23332.86734940 .00011252 00000-0 93789-3 0 9995
2 40024 98.0517 292.6012 0012177 88.8548 271.4068 14.98736011513055
| Epoch (UTC): | 28 November 2023 20:48:58 |
| Eccentricity: | 0.0012177 |
| inclination: | 98.0517° |
| perigee height: | 562 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 292.6012° |
| argument of perigee: | 88.8548° |
| revolutions per day: | 14.98736011 |
| mean anomaly at epoch: | 271.4068° |
| orbit number at epoch: | 51305 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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