View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26635U 00080A 18310.66002362 0.00000000 00000-0 00000-0 0 01
2 26635 8.4917 33.2447 0005338 202.5378 157.4501 1.00270000 05
| Epoch (UTC): | 06 November 2018 15:50:26 |
| Eccentricity: | 0.0005338 |
| inclination: | 8.4917° |
| perigee height: | 35764 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 33.2447° |
| argument of perigee: | 202.5378° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 157.4501° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|