View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54656U 26145.51299988 +.00000000 +00000-0 +22821-3 0 00006
2 54656 87.9260 248.4813 0002234 111.3961 248.7411 13.21826214 00
| Epoch (UTC): | 25 May 2026 12:18:43 |
| Eccentricity: | 0.0002234 |
| inclination: | 87.9260° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4813° |
| argument of perigee: | 111.3961° |
| revolutions per day: | 13.21826214 |
| mean anomaly at epoch: | 248.7411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|