View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25544U 26156.77317083 +.00000000 +00000-0 +17151-3 0 00007
2 25544 51.6332 356.5983 0007059 137.5864 222.5671 15.49621928 08
| Epoch (UTC): | 05 June 2026 18:33:21 |
| Eccentricity: | 0.0007059 |
| inclination: | 51.6332° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 356.5983° |
| argument of perigee: | 137.5864° |
| revolutions per day: | 15.49621928 |
| mean anomaly at epoch: | 222.5671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|