View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00082U 26047.14612219 +.00000000 +00000-0 +26168-3 0 00004
2 00082 38.8565 89.3839 1167123 0.0455 0.0196 12.27859294 07
| Epoch (UTC): | 16 February 2026 03:30:24 |
| Eccentricity: | 0.1167123 |
| inclination: | 38.8565° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 89.3839° |
| argument of perigee: | 0.0455° |
| revolutions per day: | 12.27859294 |
| mean anomaly at epoch: | 0.0196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|