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 28895U 05043F 23159.87918130 .00001779 00000-0 33557-3 0 9991
2 28895 98.1530 292.0029 0017594 98.5741 261.7457 14.65642295939821
| Epoch (UTC): | 08 June 2023 21:06:01 |
| Eccentricity: | 0.0017594 |
| inclination: | 98.1530° |
| perigee height: | 662 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 292.0029° |
| argument of perigee: | 98.5741° |
| revolutions per day: | 14.65642295 |
| mean anomaly at epoch: | 261.7457° |
| orbit number at epoch: | 93982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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