View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61567U 26145.55017096 +.00000000 +00000-0 +25435-3 0 00001
2 61567 88.9808 59.8786 0005945 148.5980 211.5556 14.02452005 07
| Epoch (UTC): | 25 May 2026 13:12:14 |
| Eccentricity: | 0.0005945 |
| inclination: | 88.9808° |
| perigee height: | 881 km |
| apogee height: | 890 km |
| right ascension of ascending node: | 59.8786° |
| argument of perigee: | 148.5980° |
| revolutions per day: | 14.02452005 |
| mean anomaly at epoch: | 211.5556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|