View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21667U 26098.21305932 +.00000000 +00000-0 -10672-4 0 00006
2 21667 82.9044 133.2377 0019218 286.7620 143.6507 13.75282354 05
| Epoch (UTC): | 08 April 2026 05:06:48 |
| Eccentricity: | 0.0019218 |
| inclination: | 82.9044° |
| perigee height: | 967 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 133.2377° |
| argument of perigee: | 286.7620° |
| revolutions per day: | 13.75282354 |
| mean anomaly at epoch: | 143.6507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|