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 28455U 02056G 24355.60488638 .00001714 00000-0 60671-3 0 9995
2 28455 98.6885 314.4997 0010767 23.2806 336.8865 14.35866199596932
| Epoch (UTC): | 20 December 2024 14:31:02 |
| Eccentricity: | 0.0010767 |
| inclination: | 98.6885° |
| perigee height: | 764 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 314.4997° |
| argument of perigee: | 23.2806° |
| revolutions per day: | 14.35866199 |
| mean anomaly at epoch: | 336.8865° |
| orbit number at epoch: | 59693 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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