View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53896U 26145.24174764 +.00000000 +00000-0 +64494-3 0 00007
2 53896 53.2133 340.3021 0001424 79.8676 280.2476 15.08780878 08
| Epoch (UTC): | 25 May 2026 05:48:06 |
| Eccentricity: | 0.0001424 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 340.3021° |
| argument of perigee: | 79.8676° |
| revolutions per day: | 15.08780878 |
| mean anomaly at epoch: | 280.2476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|