View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65046U 26145.58717054 +.00000000 +00000-0 +86927-4 0 00005
2 65046 50.0004 346.7654 0000481 50.2988 309.7926 13.29322772 06
| Epoch (UTC): | 25 May 2026 14:05:31 |
| Eccentricity: | 0.0000481 |
| inclination: | 50.0004° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 346.7654° |
| argument of perigee: | 50.2988° |
| revolutions per day: | 13.29322772 |
| mean anomaly at epoch: | 309.7926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|