View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23088U 26064.47339706 +.00000000 +00000-0 -54485-4 0 00002
2 23088 70.9986 79.7425 0005672 289.7929 70.2581 14.15013187 06
| Epoch (UTC): | 05 March 2026 11:21:41 |
| Eccentricity: | 0.0005672 |
| inclination: | 70.9986° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 79.7425° |
| argument of perigee: | 289.7929° |
| revolutions per day: | 14.15013187 |
| mean anomaly at epoch: | 70.2581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|