View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04159U 26064.16482478 +.00000000 +00000-0 +87922-4 0 00002
2 04159 69.9604 82.1056 0111859 88.6890 272.7015 13.72893370 08
| Epoch (UTC): | 05 March 2026 03:57:20 |
| Eccentricity: | 0.0111859 |
| inclination: | 69.9604° |
| perigee height: | 907 km |
| apogee height: | 1072 km |
| right ascension of ascending node: | 82.1056° |
| argument of perigee: | 88.6890° |
| revolutions per day: | 13.72893370 |
| mean anomaly at epoch: | 272.7015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|