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 23275.86692029 .00007497 00000-0 96812-3 0 9996
2 00107 28.7896 218.3404 0530523 317.6133 38.4600 14.12924993136098
| Epoch (UTC): | 02 October 2023 20:48:21 |
| Eccentricity: | 0.0530523 |
| inclination: | 28.7896° |
| perigee height: | 466 km |
| apogee height: | 1233 km |
| right ascension of ascending node: | 218.3404° |
| argument of perigee: | 317.6133° |
| revolutions per day: | 14.12924993 |
| mean anomaly at epoch: | 38.4600° |
| orbit number at epoch: | 13609 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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