View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61520U 26145.22826508 +.00000000 +00000-0 +37192-4 0 00004
2 61520 53.1596 146.7256 0001522 79.7660 280.3512 15.30195110 08
| Epoch (UTC): | 25 May 2026 05:28:42 |
| Eccentricity: | 0.0001522 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.7256° |
| argument of perigee: | 79.7660° |
| revolutions per day: | 15.30195110 |
| mean anomaly at epoch: | 280.3512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|