View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42691U 26145.60667279 +.00000000 +00000-0 +00000-0 0 00006
2 42691 0.0199 347.7273 0000738 75.7116 154.0623 1.00271982 02
| Epoch (UTC): | 25 May 2026 14:33:36 |
| Eccentricity: | 0.0000738 |
| inclination: | 0.0199° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 347.7273° |
| argument of perigee: | 75.7116° |
| revolutions per day: | 1.00271982 |
| mean anomaly at epoch: | 154.0623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|