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 00107U 61013A 23339.99311305 .00002524 00000-0 30865-3 0 9998
2 00107 28.7869 213.6347 0527369 188.3201 170.8324 14.13762594145176
| Epoch (UTC): | 05 December 2023 23:50:04 |
| Eccentricity: | 0.0527369 |
| inclination: | 28.7869° |
| perigee height: | 465 km |
| apogee height: | 1227 km |
| right ascension of ascending node: | 213.6347° |
| argument of perigee: | 188.3201° |
| revolutions per day: | 14.13762594 |
| mean anomaly at epoch: | 170.8324° |
| orbit number at epoch: | 14517 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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