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 25397U 98043D 22342.57152267 .00000084 00000-0 56732-4 0 9997
2 25397 98.8424 293.6837 0001169 16.6871 343.4345 14.23792958268201
| Epoch (UTC): | 08 December 2022 13:42:59 |
| Eccentricity: | 0.0001169 |
| inclination: | 98.8424° |
| perigee height: | 812 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 293.6837° |
| argument of perigee: | 16.6871° |
| revolutions per day: | 14.23792958 |
| mean anomaly at epoch: | 343.4345° |
| orbit number at epoch: | 26820 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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