View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 35933U 26073.57075262 +.00000000 +00000-0 +25066-3 0 00000
2 35933 98.4024 339.6305 0005650 148.8301 211.3235 14.61546162 05
| Epoch (UTC): | 14 March 2026 13:41:53 |
| Eccentricity: | 0.0005650 |
| inclination: | 98.4024° |
| perigee height: | 684 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 339.6305° |
| argument of perigee: | 148.8301° |
| revolutions per day: | 14.61546162 |
| mean anomaly at epoch: | 211.3235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|