View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50172U 26145.33512664 +.00000000 +00000-0 +30019-4 0 00003
2 50172 53.2126 265.0475 0001122 78.1855 281.9263 15.08838457 05
| Epoch (UTC): | 25 May 2026 08:02:34 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 265.0475° |
| argument of perigee: | 78.1855° |
| revolutions per day: | 15.08838457 |
| mean anomaly at epoch: | 281.9263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|