View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46039U 26145.24184042 +.00000000 +00000-0 +33440-4 0 00006
2 46039 53.1593 131.1229 0001127 81.7803 278.3326 15.30191585 06
| Epoch (UTC): | 25 May 2026 05:48:15 |
| Eccentricity: | 0.0001127 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.1229° |
| argument of perigee: | 81.7803° |
| revolutions per day: | 15.30191585 |
| mean anomaly at epoch: | 278.3326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|