View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60542U 26145.17409649 +.00000000 +00000-0 +43503-3 0 00006
2 60542 97.6654 224.5206 0003558 173.3284 186.7990 15.03852107 08
| Epoch (UTC): | 25 May 2026 04:10:41 |
| Eccentricity: | 0.0003558 |
| inclination: | 97.6654° |
| perigee height: | 553 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 224.5206° |
| argument of perigee: | 173.3284° |
| revolutions per day: | 15.03852107 |
| mean anomaly at epoch: | 186.7990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|