View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60132U 26145.39751419 +.00000000 +00000-0 +11078-3 0 00002
2 60132 53.1630 28.0328 0001694 88.2179 271.9016 15.30190940 08
| Epoch (UTC): | 25 May 2026 09:32:25 |
| Eccentricity: | 0.0001694 |
| inclination: | 53.1630° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 28.0328° |
| argument of perigee: | 88.2179° |
| revolutions per day: | 15.30190940 |
| mean anomaly at epoch: | 271.9016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|