View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21263U 26066.15861238 +.00000000 +00000-0 +85119-4 0 00009
2 21263 98.6152 56.1993 0013069 330.8953 29.1497 14.26716584 06
| Epoch (UTC): | 07 March 2026 03:48:24 |
| Eccentricity: | 0.0013069 |
| inclination: | 98.6152° |
| perigee height: | 793 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 56.1993° |
| argument of perigee: | 330.8953° |
| revolutions per day: | 14.26716584 |
| mean anomaly at epoch: | 29.1497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|