View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49062U 26145.46054689 +.00000000 +00000-0 +00000-0 0 00004
2 49062 0.0107 327.0924 0002085 164.8598 14.9295 1.00267008 08
| Epoch (UTC): | 25 May 2026 11:03:11 |
| Eccentricity: | 0.0002085 |
| inclination: | 0.0107° |
| perigee height: | 35779 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 327.0924° |
| argument of perigee: | 164.8598° |
| revolutions per day: | 1.00267008 |
| mean anomaly at epoch: | 14.9295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|