View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60476U 26145.20542691 +.00000000 +00000-0 +47856-3 0 00006
2 60476 97.3772 231.2161 0000632 350.7443 9.3795 15.45992371 02
| Epoch (UTC): | 25 May 2026 04:55:48 |
| Eccentricity: | 0.0000632 |
| inclination: | 97.3772° |
| perigee height: | 428 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 231.2161° |
| argument of perigee: | 350.7443° |
| revolutions per day: | 15.45992371 |
| mean anomaly at epoch: | 9.3795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|