View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15774U 26098.32954571 +.00000000 +00000-0 +11438-3 0 00008
2 15774 66.5868 224.9009 0026371 343.0467 44.4734 14.25353235 06
| Epoch (UTC): | 08 April 2026 07:54:32 |
| Eccentricity: | 0.0026371 |
| inclination: | 66.5868° |
| perigee height: | 788 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 224.9009° |
| argument of perigee: | 343.0467° |
| revolutions per day: | 14.25353235 |
| mean anomaly at epoch: | 44.4734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|