View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50469U 26145.34192714 +.00000000 +00000-0 -66759-4 0 00004
2 50469 87.9154 10.4116 0002195 89.0007 271.1376 13.17650765 02
| Epoch (UTC): | 25 May 2026 08:12:22 |
| Eccentricity: | 0.0002195 |
| inclination: | 87.9154° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4116° |
| argument of perigee: | 89.0007° |
| revolutions per day: | 13.17650765 |
| mean anomaly at epoch: | 271.1376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|