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 24834U 97029A 23082.98526833 -.00000138 00000-0 00000+0 0 9999
2 24834 15.0662 14.2204 0099262 208.7159 334.8869 0.96051381 92045
| Epoch (UTC): | 23 March 2023 23:38:47 |
| Eccentricity: | 0.0099262 |
| inclination: | 15.0662° |
| perigee height: | 36582 km |
| apogee height: | 37443 km |
| right ascension of ascending node: | 14.2204° |
| argument of perigee: | 208.7159° |
| revolutions per day: | 0.96051381 |
| mean anomaly at epoch: | 334.8869° |
| orbit number at epoch: | 9204 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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