View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65165U 26145.60944505 +.00000000 +00000-0 +18414-4 0 00009
2 65165 86.4920 259.5275 0001867 98.2018 261.9328 13.24404407 09
| Epoch (UTC): | 25 May 2026 14:37:36 |
| Eccentricity: | 0.0001867 |
| inclination: | 86.4920° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.5275° |
| argument of perigee: | 98.2018° |
| revolutions per day: | 13.24404407 |
| mean anomaly at epoch: | 261.9328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|