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 27945U 03042G 18267.38143509 -.00000012 +00000-0 +65697-5 0 9995
2 27945 098.0099 040.0095 0011384 214.6569 145.3893 14.64806000801003
| Epoch (UTC): | 24 September 2018 09:09:15 |
| Eccentricity: | 0.0011384 |
| inclination: | 98.0099° |
| perigee height: | 669 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 40.0095° |
| argument of perigee: | 214.6569° |
| revolutions per day: | 14.64806000 |
| mean anomaly at epoch: | 145.3893° |
| orbit number at epoch: | 80100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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