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 24357.89617359 .00009191 00000-0 11440-2 0 9990
2 00107 28.7831 188.6369 0510796 127.2569 237.5713 14.17956255199473
| Epoch (UTC): | 22 December 2024 21:30:29 |
| Eccentricity: | 0.0510796 |
| inclination: | 28.7831° |
| perigee height: | 464 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 188.6369° |
| argument of perigee: | 127.2569° |
| revolutions per day: | 14.17956255 |
| mean anomaly at epoch: | 237.5713° |
| orbit number at epoch: | 19947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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