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 25501U 98058A 18345.53039560 -.00000075 00000-0 00000+0 0 9997
2 25501 8.5029 31.5742 0014026 297.4857 47.9186 0.98176972 72942
| Epoch (UTC): | 11 December 2018 12:43:46 |
| Eccentricity: | 0.0014026 |
| inclination: | 8.5029° |
| perigee height: | 36324 km |
| apogee height: | 36444 km |
| right ascension of ascending node: | 31.5742° |
| argument of perigee: | 297.4857° |
| revolutions per day: | 0.98176972 |
| mean anomaly at epoch: | 47.9186° |
| orbit number at epoch: | 7294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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