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 23156.41733001 -.00000037 00000-0 64633-5 0 9990
2 24298 70.8265 146.0954 0017712 194.0433 166.0197 14.12516165379276
| Epoch (UTC): | 05 June 2023 10:00:57 |
| Eccentricity: | 0.0017712 |
| inclination: | 70.8265° |
| perigee height: | 838 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 146.0954° |
| argument of perigee: | 194.0433° |
| revolutions per day: | 14.12516165 |
| mean anomaly at epoch: | 166.0197° |
| orbit number at epoch: | 37927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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