View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53422U 26145.23898294 +.00000000 +00000-0 +18118-3 0 00004
2 53422 53.2132 130.4770 0001224 84.1168 275.9963 15.08851591 07
| Epoch (UTC): | 25 May 2026 05:44:08 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 130.4770° |
| argument of perigee: | 84.1168° |
| revolutions per day: | 15.08851591 |
| mean anomaly at epoch: | 275.9963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|