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 22147.67596102 .00001437 00000-0 17428-3 0 9991
2 00107 28.7851 133.9593 0542481 109.6693 256.3218 14.10067861 66364
| Epoch (UTC): | 27 May 2022 16:13:23 |
| Eccentricity: | 0.0542481 |
| inclination: | 28.7851° |
| perigee height: | 466 km |
| apogee height: | 1252 km |
| right ascension of ascending node: | 133.9593° |
| argument of perigee: | 109.6693° |
| revolutions per day: | 14.10067861 |
| mean anomaly at epoch: | 256.3218° |
| orbit number at epoch: | 6636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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