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 23036.59422571 .00004018 00000-0 51327-3 0 9992
2 00107 28.7912 136.4602 0537456 277.9412 76.0521 14.11288022102242
| Epoch (UTC): | 05 February 2023 14:15:41 |
| Eccentricity: | 0.0537456 |
| inclination: | 28.7912° |
| perigee height: | 466 km |
| apogee height: | 1244 km |
| right ascension of ascending node: | 136.4602° |
| argument of perigee: | 277.9412° |
| revolutions per day: | 14.11288022 |
| mean anomaly at epoch: | 76.0521° |
| orbit number at epoch: | 10224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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