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 23343.59333797 .00001763 00000-0 20809-3 0 9999
2 00107 28.7878 193.1472 0527354 221.5153 134.4194 14.13774683145686
| Epoch (UTC): | 09 December 2023 14:14:24 |
| Eccentricity: | 0.0527354 |
| inclination: | 28.7878° |
| perigee height: | 465 km |
| apogee height: | 1227 km |
| right ascension of ascending node: | 193.1472° |
| argument of perigee: | 221.5153° |
| revolutions per day: | 14.13774683 |
| mean anomaly at epoch: | 134.4194° |
| orbit number at epoch: | 14568 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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