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 27431U 02024B 19081.95668028 .00000057 00000-0 58575-4 0 9994
2 27431 99.1107 68.8363 0016463 86.1094 274.1957 14.09672273867106
| Epoch (UTC): | 22 March 2019 22:57:37 |
| Eccentricity: | 0.0016463 |
| inclination: | 99.1107° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 68.8363° |
| argument of perigee: | 86.1094° |
| revolutions per day: | 14.09672273 |
| mean anomaly at epoch: | 274.1957° |
| orbit number at epoch: | 86710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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