View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33396U 26088.14209920 +.00000000 +00000-0 +99257-4 0 00004
2 33396 98.5663 147.9954 0001075 97.0580 263.0719 14.20121080 01
| Epoch (UTC): | 29 March 2026 03:24:37 |
| Eccentricity: | 0.0001075 |
| inclination: | 98.5663° |
| perigee height: | 824 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 147.9954° |
| argument of perigee: | 97.0580° |
| revolutions per day: | 14.20121080 |
| mean anomaly at epoch: | 263.0719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|