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 24282.64547574 .00017632 00000-0 30143-2 0 9996
2 28895 98.2181 58.8134 0015144 2.6356 357.4926 14.68852069 11332
| Epoch (UTC): | 08 October 2024 15:29:29 |
| Eccentricity: | 0.0015144 |
| inclination: | 98.2181° |
| perigee height: | 654 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 58.8134° |
| argument of perigee: | 2.6356° |
| revolutions per day: | 14.68852069 |
| mean anomaly at epoch: | 357.4926° |
| orbit number at epoch: | 1133 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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