View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33499U 26101.46103566 +.00000000 +00000-0 +15219-3 0 00003
2 33499 98.1187 22.8576 0008714 138.6010 221.5865 14.82953873 02
| Epoch (UTC): | 11 April 2026 11:03:53 |
| Eccentricity: | 0.0008714 |
| inclination: | 98.1187° |
| perigee height: | 614 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 22.8576° |
| argument of perigee: | 138.6010° |
| revolutions per day: | 14.82953873 |
| mean anomaly at epoch: | 221.5865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|