View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12786U 26101.44717302 +.00000000 +00000-0 +31881-4 0 00000
2 12786 82.4897 169.6184 0018048 58.1985 302.0987 14.87177260 08
| Epoch (UTC): | 11 April 2026 10:43:55 |
| Eccentricity: | 0.0018048 |
| inclination: | 82.4897° |
| perigee height: | 594 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 169.6184° |
| argument of perigee: | 58.1985° |
| revolutions per day: | 14.87177260 |
| mean anomaly at epoch: | 302.0987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|