View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61604U 26145.38990455 +.00000000 +00000-0 -15308-2 0 00001
2 61604 87.8907 25.6174 0001117 41.4519 318.6694 13.11417337 05
| Epoch (UTC): | 25 May 2026 09:21:27 |
| Eccentricity: | 0.0001117 |
| inclination: | 87.8907° |
| perigee height: | 1217 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6174° |
| argument of perigee: | 41.4519° |
| revolutions per day: | 13.11417337 |
| mean anomaly at epoch: | 318.6694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|