View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27640U 26140.29296117 +.00000000 +00000-0 +42115-4 0 00009
2 27640 98.7133 147.6035 0012881 295.5078 64.4766 14.19936382 03
| Epoch (UTC): | 20 May 2026 07:01:51 |
| Eccentricity: | 0.0012881 |
| inclination: | 98.7133° |
| perigee height: | 816 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 147.6035° |
| argument of perigee: | 295.5078° |
| revolutions per day: | 14.19936382 |
| mean anomaly at epoch: | 64.4766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|