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 23079.68138890 .00000001 00000-0 40282-4 0 9993
2 24278 98.5223 70.3233 0349203 286.5559 69.7500 13.53138828312963
| Epoch (UTC): | 20 March 2023 16:21:12 |
| Eccentricity: | 0.0349203 |
| inclination: | 98.5223° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 70.3233° |
| argument of perigee: | 286.5559° |
| revolutions per day: | 13.53138828 |
| mean anomaly at epoch: | 69.7500° |
| orbit number at epoch: | 31296 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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