View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60380U 26145.54976477 +.00000000 +00000-0 +12665-3 0 00000
2 60380 88.9701 282.0959 0014608 78.4068 281.8722 13.51005940 07
| Epoch (UTC): | 25 May 2026 13:11:39 |
| Eccentricity: | 0.0014608 |
| inclination: | 88.9701° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 282.0959° |
| argument of perigee: | 78.4068° |
| revolutions per day: | 13.51005940 |
| mean anomaly at epoch: | 281.8722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|