View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22803U 26076.17026169 +.00000000 +00000-0 +12741-3 0 00009
2 22803 70.9931 355.3525 0018098 205.5630 154.4601 14.17232447 07
| Epoch (UTC): | 17 March 2026 04:05:10 |
| Eccentricity: | 0.0018098 |
| inclination: | 70.9931° |
| perigee height: | 822 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 355.3525° |
| argument of perigee: | 205.5630° |
| revolutions per day: | 14.17232447 |
| mean anomaly at epoch: | 154.4601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|