View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27058U 26065.80007014 +.00000000 +00000-0 +22212-4 0 00007
2 27058 82.5291 267.5222 0002391 217.1608 142.9317 12.62084219 09
| Epoch (UTC): | 06 March 2026 19:12:06 |
| Eccentricity: | 0.0002391 |
| inclination: | 82.5291° |
| perigee height: | 1412 km |
| apogee height: | 1416 km |
| right ascension of ascending node: | 267.5222° |
| argument of perigee: | 217.1608° |
| revolutions per day: | 12.62084219 |
| mean anomaly at epoch: | 142.9317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|