View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61940U 26145.29604635 +.00000000 +00000-0 +20185-2 0 00004
2 61940 53.1575 353.3396 0001156 65.8923 294.2216 15.69806543 09
| Epoch (UTC): | 25 May 2026 07:06:18 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.1575° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 353.3396° |
| argument of perigee: | 65.8923° |
| revolutions per day: | 15.69806543 |
| mean anomaly at epoch: | 294.2216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|