View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49505U 26145.60953280 +.00000000 +00000-0 +00000-0 0 00007
2 49505 0.0365 87.3638 0000772 122.5357 22.8946 1.00273518 03
| Epoch (UTC): | 25 May 2026 14:37:43 |
| Eccentricity: | 0.0000772 |
| inclination: | 0.0365° |
| perigee height: | 35783 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 87.3638° |
| argument of perigee: | 122.5357° |
| revolutions per day: | 1.00273518 |
| mean anomaly at epoch: | 22.8946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|