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 22146.68493355 .00001571 00000-0 19266-3 0 9998
2 00107 28.7849 139.5665 0542493 100.5908 265.6210 14.10065422 66226
| Epoch (UTC): | 26 May 2022 16:26:18 |
| Eccentricity: | 0.0542493 |
| inclination: | 28.7849° |
| perigee height: | 466 km |
| apogee height: | 1252 km |
| right ascension of ascending node: | 139.5665° |
| argument of perigee: | 100.5908° |
| revolutions per day: | 14.10065422 |
| mean anomaly at epoch: | 265.6210° |
| orbit number at epoch: | 6622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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