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 25940U 99057A 18352.84604289 .00000013 00000-0 19786-4 0 9999
2 25940 98.5480 290.7240 0005324 157.6007 202.5412 14.35452172 4688
| Epoch (UTC): | 18 December 2018 20:18:18 |
| Eccentricity: | 0.0005324 |
| inclination: | 98.5480° |
| perigee height: | 770 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 290.7240° |
| argument of perigee: | 157.6007° |
| revolutions per day: | 14.35452172 |
| mean anomaly at epoch: | 202.5412° |
| orbit number at epoch: | 468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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