View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23405U 26072.93639216 +.00000000 +00000-0 +12154-3 0 00009
2 23405 70.9852 343.5559 0002856 206.7335 153.3641 14.15562299 05
| Epoch (UTC): | 13 March 2026 22:28:24 |
| Eccentricity: | 0.0002856 |
| inclination: | 70.9852° |
| perigee height: | 838 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 343.5559° |
| argument of perigee: | 206.7335° |
| revolutions per day: | 14.15562299 |
| mean anomaly at epoch: | 153.3641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|