View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69083U 26145.59716094 +.00000000 +00000-0 +62423-4 0 00009
2 69083 88.9867 344.1962 0003873 164.4858 195.6455 14.25596738 05
| Epoch (UTC): | 25 May 2026 14:19:54 |
| Eccentricity: | 0.0003873 |
| inclination: | 88.9867° |
| perigee height: | 804 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 344.1962° |
| argument of perigee: | 164.4858° |
| revolutions per day: | 14.25596738 |
| mean anomaly at epoch: | 195.6455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|