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 24297U 96051A 23152.45848782 .00000124 00000-0 91210-4 0 9998
2 24297 70.9042 155.6723 0023775 187.3225 172.7553 14.13470827379184
| Epoch (UTC): | 01 June 2023 11:00:13 |
| Eccentricity: | 0.0023775 |
| inclination: | 70.9042° |
| perigee height: | 830 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 155.6723° |
| argument of perigee: | 187.3225° |
| revolutions per day: | 14.13470827 |
| mean anomaly at epoch: | 172.7553° |
| orbit number at epoch: | 37918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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