View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54824U 26145.11907654 +.00000000 +00000-0 +25291-4 0 00000
2 54824 43.0048 64.3074 0001049 238.5264 121.5485 15.27581336 09
| Epoch (UTC): | 25 May 2026 02:51:28 |
| Eccentricity: | 0.0001049 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.3074° |
| argument of perigee: | 238.5264° |
| revolutions per day: | 15.27581336 |
| mean anomaly at epoch: | 121.5485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|