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 23080.51145277 .00002498 00000-0 31143-3 0 9992
2 00107 28.7888 247.4478 0535985 321.2612 35.0664 14.11640738108456
| Epoch (UTC): | 21 March 2023 12:16:29 |
| Eccentricity: | 0.0535985 |
| inclination: | 28.7888° |
| perigee height: | 466 km |
| apogee height: | 1241 km |
| right ascension of ascending node: | 247.4478° |
| argument of perigee: | 321.2612° |
| revolutions per day: | 14.11640738 |
| mean anomaly at epoch: | 35.0664° |
| orbit number at epoch: | 10845 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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