View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42471U 26064.93023154 +.00000000 +00000-0 +22478-2 0 00001
2 42471 26.4808 337.9065 7456964 76.6036 349.8501 1.89255665 07
| Epoch (UTC): | 05 March 2026 22:19:32 |
| Eccentricity: | 0.7456964 |
| inclination: | 26.4808° |
| perigee height: | 643 km |
| apogee height: | 41817 km |
| right ascension of ascending node: | 337.9065° |
| argument of perigee: | 76.6036° |
| revolutions per day: | 1.89255665 |
| mean anomaly at epoch: | 349.8501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|