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 23151.46018331 -.00000012 00000-0 19727-4 0 9998
2 24298 70.8264 156.5534 0018047 200.6902 159.3490 14.12515839378572
| Epoch (UTC): | 31 May 2023 11:02:39 |
| Eccentricity: | 0.0018047 |
| inclination: | 70.8264° |
| perigee height: | 838 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 156.5534° |
| argument of perigee: | 200.6902° |
| revolutions per day: | 14.12515839 |
| mean anomaly at epoch: | 159.3490° |
| orbit number at epoch: | 37857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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