View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57247U 26144.79638383 +.00000000 +00000-0 +34023-4 0 00008
2 57247 43.0030 309.7214 0001680 265.1311 94.9349 15.27576034 05
| Epoch (UTC): | 24 May 2026 19:06:47 |
| Eccentricity: | 0.0001680 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.7214° |
| argument of perigee: | 265.1311° |
| revolutions per day: | 15.27576034 |
| mean anomaly at epoch: | 94.9349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|