View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25544U 26069.15865509 +.00000000 +00000-0 +17626-3 0 00000
2 25544 51.6324 70.0375 0007972 176.2903 183.8146 15.48557200 06
| Epoch (UTC): | 10 March 2026 03:48:27 |
| Eccentricity: | 0.0007972 |
| inclination: | 51.6324° |
| perigee height: | 416 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 70.0375° |
| argument of perigee: | 176.2903° |
| revolutions per day: | 15.48557200 |
| mean anomaly at epoch: | 183.8146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|