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 28975U 87001C 22183.17241067 .00000635 00000-0 44029-3 0 9997
2 28975 82.4617 124.7169 0019558 119.5216 307.2217 13.97507456460597
| Epoch (UTC): | 02 July 2022 04:08:16 |
| Eccentricity: | 0.0019558 |
| inclination: | 82.4617° |
| perigee height: | 888 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 124.7169° |
| argument of perigee: | 119.5216° |
| revolutions per day: | 13.97507456 |
| mean anomaly at epoch: | 307.2217° |
| orbit number at epoch: | 46059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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