View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55802U 26145.32937674 +.00000000 +00000-0 +61976-3 0 00004
2 55802 87.8933 294.3126 0002230 86.4992 273.6393 13.14501653 04
| Epoch (UTC): | 25 May 2026 07:54:18 |
| Eccentricity: | 0.0002230 |
| inclination: | 87.8933° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.3126° |
| argument of perigee: | 86.4992° |
| revolutions per day: | 13.14501653 |
| mean anomaly at epoch: | 273.6393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|