View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21949U 26138.16670719 +.00000000 +00000-0 +35396-4 0 00005
2 21949 85.0062 91.3320 0002232 108.8258 251.3177 14.32388742 05
| Epoch (UTC): | 18 May 2026 04:00:03 |
| Eccentricity: | 0.0002232 |
| inclination: | 85.0062° |
| perigee height: | 782 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 91.3320° |
| argument of perigee: | 108.8258° |
| revolutions per day: | 14.32388742 |
| mean anomaly at epoch: | 251.3177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|