View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22698U 26156.80901383 +.00000000 +00000-0 +47801-4 0 00006
2 22698 89.5025 60.9836 0086548 222.3436 137.1055 14.24183977 01
| Epoch (UTC): | 05 June 2026 19:24:58 |
| Eccentricity: | 0.0086548 |
| inclination: | 89.5025° |
| perigee height: | 749 km |
| apogee height: | 873 km |
| right ascension of ascending node: | 60.9836° |
| argument of perigee: | 222.3436° |
| revolutions per day: | 14.24183977 |
| mean anomaly at epoch: | 137.1055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|