View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14208U 26069.46762440 +.00000000 +00000-0 +35731-3 0 00006
2 14208 97.6147 74.0742 0020199 222.9243 137.0426 15.38440575 05
| Epoch (UTC): | 10 March 2026 11:13:22 |
| Eccentricity: | 0.0020199 |
| inclination: | 97.6147° |
| perigee height: | 437 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 74.0742° |
| argument of perigee: | 222.9243° |
| revolutions per day: | 15.38440575 |
| mean anomaly at epoch: | 137.0426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|