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 23087.22339291 .00000035 00000-0 74910-4 0 9992
2 24278 98.5233 76.8331 0349186 266.9258 89.1882 13.53139696314237
| Epoch (UTC): | 28 March 2023 05:21:41 |
| Eccentricity: | 0.0349186 |
| inclination: | 98.5233° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 76.8331° |
| argument of perigee: | 266.9258° |
| revolutions per day: | 13.53139696 |
| mean anomaly at epoch: | 89.1882° |
| orbit number at epoch: | 31423 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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