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 23268.41073068 .00017421 00000-0 15027-2 0 9993
2 40024 98.0363 226.1881 0009401 316.2040 43.8434 14.97319109503401
| Epoch (UTC): | 25 September 2023 09:51:27 |
| Eccentricity: | 0.0009401 |
| inclination: | 98.0363° |
| perigee height: | 568 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 226.1881° |
| argument of perigee: | 316.2040° |
| revolutions per day: | 14.97319109 |
| mean anomaly at epoch: | 43.8434° |
| orbit number at epoch: | 50340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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