View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08520U 26064.13196683 +.00000000 +00000-0 +15922-3 0 00005
2 08520 81.2903 330.3115 0028284 347.3755 12.6703 14.09420554 07
| Epoch (UTC): | 05 March 2026 03:10:01 |
| Eccentricity: | 0.0028284 |
| inclination: | 81.2903° |
| perigee height: | 841 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 330.3115° |
| argument of perigee: | 347.3755° |
| revolutions per day: | 14.09420554 |
| mean anomaly at epoch: | 12.6703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|