View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10521U 26045.77374227 +.00000000 +00000-0 +95328-4 0 00009
2 10521 74.0275 166.0314 0019394 129.3295 230.9584 14.42378546 09
| Epoch (UTC): | 14 February 2026 18:34:11 |
| Eccentricity: | 0.0019394 |
| inclination: | 74.0275° |
| perigee height: | 737 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 166.0314° |
| argument of perigee: | 129.3295° |
| revolutions per day: | 14.42378546 |
| mean anomaly at epoch: | 230.9584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|