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 21809U 91076E 18158.05379397 0.00000000 00000-0 00000-0 0 02
2 21809 63.3572 261.2136 0779000 26.1039 333.8961 13.41415939 06
| Epoch (UTC): | 07 June 2018 01:17:27 |
| Eccentricity: | 0.0779000 |
| inclination: | 63.3572° |
| perigee height: | 521 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 261.2136° |
| argument of perigee: | 26.1039° |
| revolutions per day: | 13.41415939 |
| mean anomaly at epoch: | 333.8961° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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