View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66831U 26145.35902905 +.00000000 +00000-0 +16512-3 0 00006
2 66831 70.0008 141.0098 0004187 263.5405 96.5277 14.98333638 03
| Epoch (UTC): | 25 May 2026 08:37:00 |
| Eccentricity: | 0.0004187 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.0098° |
| argument of perigee: | 263.5405° |
| revolutions per day: | 14.98333638 |
| mean anomaly at epoch: | 96.5277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|