View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60543U 26145.18338041 +.00000000 +00000-0 +75864-4 0 00001
2 60543 97.6806 216.3055 0002653 150.2093 209.9276 14.89810920 01
| Epoch (UTC): | 25 May 2026 04:24:04 |
| Eccentricity: | 0.0002653 |
| inclination: | 97.6806° |
| perigee height: | 597 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 216.3055° |
| argument of perigee: | 150.2093° |
| revolutions per day: | 14.89810920 |
| mean anomaly at epoch: | 209.9276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|