View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58660U 26145.61321259 +.00000000 +00000-0 +26450-3 0 00005
2 58660 97.4476 261.8078 0005763 50.7792 309.3960 15.31172334 07
| Epoch (UTC): | 25 May 2026 14:43:01 |
| Eccentricity: | 0.0005763 |
| inclination: | 97.4476° |
| perigee height: | 468 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 261.8078° |
| argument of perigee: | 50.7792° |
| revolutions per day: | 15.31172334 |
| mean anomaly at epoch: | 309.3960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|