View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00022U 26037.42865448 +.00000000 +00000-0 +76535-3 0 00005
2 00022 50.2460 25.3338 0083917 318.4288 41.0310 15.25568799 05
| Epoch (UTC): | 06 February 2026 10:17:15 |
| Eccentricity: | 0.0083917 |
| inclination: | 50.2460° |
| perigee height: | 431 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 25.3338° |
| argument of perigee: | 318.4288° |
| revolutions per day: | 15.25568799 |
| mean anomaly at epoch: | 41.0310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|