View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25405U 26159.09211074 +.00000000 +00000-0 -21327-5 0 00007
2 25405 19.0986 0.3351 7169846 77.1944 348.2423 2.25770257 09
| Epoch (UTC): | 08 June 2026 02:12:38 |
| Eccentricity: | 0.7169846 |
| inclination: | 19.0986° |
| perigee height: | 568 km |
| apogee height: | 35765 km |
| right ascension of ascending node: | 0.3351° |
| argument of perigee: | 77.1944° |
| revolutions per day: | 2.25770257 |
| mean anomaly at epoch: | 348.2423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|