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 24276.85493787 .00010808 00000-0 18575-2 0 9991
2 28895 98.2167 52.9930 0015398 20.8627 339.3203 14.68739852 10485
| Epoch (UTC): | 02 October 2024 20:31:06 |
| Eccentricity: | 0.0015398 |
| inclination: | 98.2167° |
| perigee height: | 654 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 52.9930° |
| argument of perigee: | 20.8627° |
| revolutions per day: | 14.68739852 |
| mean anomaly at epoch: | 339.3203° |
| orbit number at epoch: | 1048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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