View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41634U 26071.20758943 +.00000000 +00000-0 +11120-3 0 00003
2 41634 75.0014 102.5162 0008672 270.1995 89.8200 14.93237061 03
| Epoch (UTC): | 12 March 2026 04:58:55 |
| Eccentricity: | 0.0008672 |
| inclination: | 75.0014° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 102.5162° |
| argument of perigee: | 270.1995° |
| revolutions per day: | 14.93237061 |
| mean anomaly at epoch: | 89.8200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|