View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50195U 26145.01588995 +.00000000 +00000-0 +81408-4 0 00001
2 50195 53.2155 256.4789 0001255 92.5468 267.5668 15.08837820 03
| Epoch (UTC): | 25 May 2026 00:22:52 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 256.4789° |
| argument of perigee: | 92.5468° |
| revolutions per day: | 15.08837820 |
| mean anomaly at epoch: | 267.5668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|