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 24278U 96046B 23153.84625521 -.00000014 00000-0 18777-4 0 9995
2 24278 98.5276 134.3570 0351308 94.0780 270.0587 13.53145315322998
| Epoch (UTC): | 02 June 2023 20:18:36 |
| Eccentricity: | 0.0351308 |
| inclination: | 98.5276° |
| perigee height: | 799 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 134.3570° |
| argument of perigee: | 94.0780° |
| revolutions per day: | 13.53145315 |
| mean anomaly at epoch: | 270.0587° |
| orbit number at epoch: | 32299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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