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 45325U 91056BP 24358.09087511 .00041495 00000-0 22003-1 0 9994
2 45325 82.5525 36.1156 0166323 236.3173 122.2047 14.06541231241255
| Epoch (UTC): | 23 December 2024 02:10:51 |
| Eccentricity: | 0.0166323 |
| inclination: | 82.5525° |
| perigee height: | 750 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 36.1156° |
| argument of perigee: | 236.3173° |
| revolutions per day: | 14.06541231 |
| mean anomaly at epoch: | 122.2047° |
| orbit number at epoch: | 24125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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