View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50504U 26145.50223464 +.00000000 +00000-0 +53270-4 0 00002
2 50504 87.9159 339.9749 0001644 85.2820 274.8499 13.18686694 04
| Epoch (UTC): | 25 May 2026 12:03:13 |
| Eccentricity: | 0.0001644 |
| inclination: | 87.9159° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9749° |
| argument of perigee: | 85.2820° |
| revolutions per day: | 13.18686694 |
| mean anomaly at epoch: | 274.8499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|