View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60549U 26145.45638021 +.00000000 +00000-0 +95202-4 0 00006
2 60549 97.6815 222.3194 0005300 140.1079 220.0534 14.97861580 00
| Epoch (UTC): | 25 May 2026 10:57:11 |
| Eccentricity: | 0.0005300 |
| inclination: | 97.6815° |
| perigee height: | 570 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 222.3194° |
| argument of perigee: | 140.1079° |
| revolutions per day: | 14.97861580 |
| mean anomaly at epoch: | 220.0534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|