View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00082U 26049.09905995 +.00000000 +00000-0 +23114-3 0 00004
2 00082 38.8558 82.1291 1166983 9.5040 352.5821 12.27860194 00
| Epoch (UTC): | 18 February 2026 02:22:38 |
| Eccentricity: | 0.1166983 |
| inclination: | 38.8558° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 82.1291° |
| argument of perigee: | 9.5040° |
| revolutions per day: | 12.27860194 |
| mean anomaly at epoch: | 352.5821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|