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 24357.82802372 .00003920 00000-0 66544-3 0 9999
2 28895 98.2242 134.4872 0015951 120.0964 240.1825 14.69693126 22141
| Epoch (UTC): | 22 December 2024 19:52:21 |
| Eccentricity: | 0.0015951 |
| inclination: | 98.2242° |
| perigee height: | 651 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 134.4872° |
| argument of perigee: | 120.0964° |
| revolutions per day: | 14.69693126 |
| mean anomaly at epoch: | 240.1825° |
| orbit number at epoch: | 2214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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