View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26770U 01020A 20185.07413062 0.00000000 00000-0 00000-0 0 07
2 26770 7.9176 43.1250 0016202 49.2544 310.8983 0.98833351 00
| Epoch (UTC): | 03 July 2020 01:46:44 |
| Eccentricity: | 0.0016202 |
| inclination: | 7.9176° |
| perigee height: | 36125 km |
| apogee height: | 36263 km |
| right ascension of ascending node: | 43.1250° |
| argument of perigee: | 49.2544° |
| revolutions per day: | 0.98833351 |
| mean anomaly at epoch: | 310.8983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|