View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21398U 26071.62994450 +.00000000 +00000-0 +54741-4 0 00006
2 21398 82.5226 133.7323 0021377 152.9375 207.2959 14.81844767 08
| Epoch (UTC): | 12 March 2026 15:07:07 |
| Eccentricity: | 0.0021377 |
| inclination: | 82.5226° |
| perigee height: | 609 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 133.7323° |
| argument of perigee: | 152.9375° |
| revolutions per day: | 14.81844767 |
| mean anomaly at epoch: | 207.2959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|