View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55970U 26144.92169741 +.00000000 +00000-0 +00000-0 0 00005
2 55970 0.0167 315.2048 0001105 23.1363 132.9008 1.00272158 09
| Epoch (UTC): | 24 May 2026 22:07:14 |
| Eccentricity: | 0.0001105 |
| inclination: | 0.0167° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 315.2048° |
| argument of perigee: | 23.1363° |
| revolutions per day: | 1.00272158 |
| mean anomaly at epoch: | 132.9008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|