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 23089.44164660 .00000043 00000-0 82196-4 0 9998
2 24278 98.5235 78.7479 0349197 261.1519 94.9939 13.53140016314530
| Epoch (UTC): | 30 March 2023 10:35:58 |
| Eccentricity: | 0.0349197 |
| inclination: | 98.5235° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 78.7479° |
| argument of perigee: | 261.1519° |
| revolutions per day: | 13.53140016 |
| mean anomaly at epoch: | 94.9939° |
| orbit number at epoch: | 31453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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