View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33398U 26088.22931610 +.00000000 +00000-0 +56662-3 0 00005
2 33398 98.8385 86.2243 0022249 93.8299 266.5461 14.91073084 00
| Epoch (UTC): | 29 March 2026 05:30:12 |
| Eccentricity: | 0.0022249 |
| inclination: | 98.8385° |
| perigee height: | 579 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 86.2243° |
| argument of perigee: | 93.8299° |
| revolutions per day: | 14.91073084 |
| mean anomaly at epoch: | 266.5461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|