View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07714U 26068.22196478 +.00000000 +00000-0 +43452-4 0 00005
2 07714 81.1954 327.1369 0028036 272.7595 87.0366 14.08463018 01
| Epoch (UTC): | 09 March 2026 05:19:37 |
| Eccentricity: | 0.0028036 |
| inclination: | 81.1954° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 327.1369° |
| argument of perigee: | 272.7595° |
| revolutions per day: | 14.08463018 |
| mean anomaly at epoch: | 87.0366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|