View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52343U 26145.63320185 +.00000000 +00000-0 -14611-3 0 00003
2 52343 53.2118 223.7083 0001160 80.8189 279.2934 15.08852515 02
| Epoch (UTC): | 25 May 2026 15:11:48 |
| Eccentricity: | 0.0001160 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 223.7083° |
| argument of perigee: | 80.8189° |
| revolutions per day: | 15.08852515 |
| mean anomaly at epoch: | 279.2934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|