View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65167U 26145.62456138 +.00000000 +00000-0 +42739-4 0 00000
2 65167 86.4960 259.6461 0002047 93.2529 266.8839 13.24404563 00
| Epoch (UTC): | 25 May 2026 14:59:22 |
| Eccentricity: | 0.0002047 |
| inclination: | 86.4960° |
| perigee height: | 1166 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.6461° |
| argument of perigee: | 93.2529° |
| revolutions per day: | 13.24404563 |
| mean anomaly at epoch: | 266.8839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|