View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00205U 26039.18282319 +.00000000 +00000-0 +43352-4 0 00005
2 00205 32.4407 83.0655 0101813 74.7636 286.4216 13.62566337 04
| Epoch (UTC): | 08 February 2026 04:23:15 |
| Eccentricity: | 0.0101813 |
| inclination: | 32.4407° |
| perigee height: | 951 km |
| apogee height: | 1102 km |
| right ascension of ascending node: | 83.0655° |
| argument of perigee: | 74.7636° |
| revolutions per day: | 13.62566337 |
| mean anomaly at epoch: | 286.4216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|