View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54836U 26145.38644513 +.00000000 +00000-0 +13612-2 0 00006
2 54836 42.9986 33.1750 0003843 261.9804 98.0641 16.08187039 04
| Epoch (UTC): | 25 May 2026 09:16:28 |
| Eccentricity: | 0.0003843 |
| inclination: | 42.9986° |
| perigee height: | 249 km |
| apogee height: | 254 km |
| right ascension of ascending node: | 33.1750° |
| argument of perigee: | 261.9804° |
| revolutions per day: | 16.08187039 |
| mean anomaly at epoch: | 98.0641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|