View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21949U 26033.38049025 +.00000000 +00000-0 +76583-4 0 00006
2 21949 85.0118 151.7994 0002451 108.8172 251.3287 14.32353753 09
| Epoch (UTC): | 02 February 2026 09:07:54 |
| Eccentricity: | 0.0002451 |
| inclination: | 85.0118° |
| perigee height: | 782 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 151.7994° |
| argument of perigee: | 108.8172° |
| revolutions per day: | 14.32353753 |
| mean anomaly at epoch: | 251.3287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|