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 22274.30530558 .00002103 00000-0 25990-3 0 9999
2 00107 28.7878 137.3799 0540696 190.2758 168.6358 14.10470017 84252
| Epoch (UTC): | 01 October 2022 07:19:38 |
| Eccentricity: | 0.0540696 |
| inclination: | 28.7878° |
| perigee height: | 466 km |
| apogee height: | 1249 km |
| right ascension of ascending node: | 137.3799° |
| argument of perigee: | 190.2758° |
| revolutions per day: | 14.10470017 |
| mean anomaly at epoch: | 168.6358° |
| orbit number at epoch: | 8425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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