View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46538U 26145.12954659 +.00000000 +00000-0 +81157-3 0 00003
2 46538 53.0345 92.8089 0006650 74.2393 285.9361 15.80086428 05
| Epoch (UTC): | 25 May 2026 03:06:32 |
| Eccentricity: | 0.0006650 |
| inclination: | 53.0345° |
| perigee height: | 326 km |
| apogee height: | 335 km |
| right ascension of ascending node: | 92.8089° |
| argument of perigee: | 74.2393° |
| revolutions per day: | 15.80086428 |
| mean anomaly at epoch: | 285.9361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|