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 23266.87368085 .00010054 00000-0 87126-3 0 9992
2 40024 98.0366 224.6073 0009588 322.3215 37.7334 14.97277960503698
| Epoch (UTC): | 23 September 2023 20:58:06 |
| Eccentricity: | 0.0009588 |
| inclination: | 98.0366° |
| perigee height: | 568 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 224.6073° |
| argument of perigee: | 322.3215° |
| revolutions per day: | 14.97277960 |
| mean anomaly at epoch: | 37.7334° |
| orbit number at epoch: | 50369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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