View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22823U 26088.20057251 +.00000000 +00000-0 +48509-4 0 00006
2 22823 98.8645 152.1165 0017751 111.3560 248.9512 14.20070066 05
| Epoch (UTC): | 29 March 2026 04:48:49 |
| Eccentricity: | 0.0017751 |
| inclination: | 98.8645° |
| perigee height: | 812 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 152.1165° |
| argument of perigee: | 111.3560° |
| revolutions per day: | 14.20070066 |
| mean anomaly at epoch: | 248.9512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|