View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60500U 26145.17969694 +.00000000 +00000-0 +31154-3 0 00000
2 60500 97.3775 226.6243 0003022 58.8407 301.3130 15.30053826 09
| Epoch (UTC): | 25 May 2026 04:18:45 |
| Eccentricity: | 0.0003022 |
| inclination: | 97.3775° |
| perigee height: | 474 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 226.6243° |
| argument of perigee: | 58.8407° |
| revolutions per day: | 15.30053826 |
| mean anomaly at epoch: | 301.3130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|