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 24298U 96051B 23153.72630763 -.00000018 00000-0 16719-4 0 9992
2 24298 70.8265 151.7727 0017895 197.7169 162.3329 14.12516023378891
| Epoch (UTC): | 02 June 2023 17:25:52 |
| Eccentricity: | 0.0017895 |
| inclination: | 70.8265° |
| perigee height: | 838 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 151.7727° |
| argument of perigee: | 197.7169° |
| revolutions per day: | 14.12516023 |
| mean anomaly at epoch: | 162.3329° |
| orbit number at epoch: | 37889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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