View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55049U 26145.61184544 +.00000000 +00000-0 +50915-3 0 00000
2 55049 97.3243 230.0136 0004458 183.8547 176.2696 15.95942274 00
| Epoch (UTC): | 25 May 2026 14:41:03 |
| Eccentricity: | 0.0004458 |
| inclination: | 97.3243° |
| perigee height: | 283 km |
| apogee height: | 289 km |
| right ascension of ascending node: | 230.0136° |
| argument of perigee: | 183.8547° |
| revolutions per day: | 15.95942274 |
| mean anomaly at epoch: | 176.2696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|