View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41166U 26145.51146568 +.00000000 +00000-0 +35595-3 0 00005
2 41166 14.9822 259.9818 0004396 251.0999 108.8850 15.48888762 02
| Epoch (UTC): | 25 May 2026 12:16:30 |
| Eccentricity: | 0.0004396 |
| inclination: | 14.9822° |
| perigee height: | 417 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 259.9818° |
| argument of perigee: | 251.0999° |
| revolutions per day: | 15.48888762 |
| mean anomaly at epoch: | 108.8850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|