View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25544U 26052.76529868 +.00000000 +00000-0 +20704-3 0 00005
2 25544 51.6320 151.0701 0008512 119.8639 240.3195 15.48189327 09
| Epoch (UTC): | 21 February 2026 18:22:01 |
| Eccentricity: | 0.0008512 |
| inclination: | 51.6320° |
| perigee height: | 416 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 151.0701° |
| argument of perigee: | 119.8639° |
| revolutions per day: | 15.48189327 |
| mean anomaly at epoch: | 240.3195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|