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 25400U 98043G 21018.85422779 -.00000004 00000-0 16863-4 0 9994
2 25400 98.6286 316.9989 0010968 69.5533 290.6823 14.25468599171701
| Epoch (UTC): | 18 January 2021 20:30:05 |
| Eccentricity: | 0.0010968 |
| inclination: | 98.6286° |
| perigee height: | 799 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 316.9989° |
| argument of perigee: | 69.5533° |
| revolutions per day: | 14.25468599 |
| mean anomaly at epoch: | 290.6823° |
| orbit number at epoch: | 17170 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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