View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 35873U 26145.04161579 +.00000000 +00000-0 +00000-0 0 00000
2 35873 0.0497 96.9324 0002945 328.6096 119.3746 1.00271735 02
| Epoch (UTC): | 25 May 2026 00:59:55 |
| Eccentricity: | 0.0002945 |
| inclination: | 0.0497° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 96.9324° |
| argument of perigee: | 328.6096° |
| revolutions per day: | 1.00271735 |
| mean anomaly at epoch: | 119.3746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|