View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60909U 26145.62918296 +.00000000 +00000-0 +46935-4 0 00009
2 60909 53.1605 112.3431 0001440 102.0960 258.0219 15.69683711 02
| Epoch (UTC): | 25 May 2026 15:06:01 |
| Eccentricity: | 0.0001440 |
| inclination: | 53.1605° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 112.3431° |
| argument of perigee: | 102.0960° |
| revolutions per day: | 15.69683711 |
| mean anomaly at epoch: | 258.0219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|