View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60459U 26145.64787806 +.00000000 +00000-0 +37024-3 0 00000
2 60459 34.9928 278.5766 0007864 3.3748 356.7023 15.35273615 06
| Epoch (UTC): | 25 May 2026 15:32:56 |
| Eccentricity: | 0.0007864 |
| inclination: | 34.9928° |
| perigee height: | 455 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 278.5766° |
| argument of perigee: | 3.3748° |
| revolutions per day: | 15.35273615 |
| mean anomaly at epoch: | 356.7023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|