View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62131U 26145.17556500 +.00000000 +00000-0 +73274-3 0 00009
2 62131 43.0032 64.4738 0001556 267.0931 92.9743 15.27601153 09
| Epoch (UTC): | 25 May 2026 04:12:48 |
| Eccentricity: | 0.0001556 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.4738° |
| argument of perigee: | 267.0931° |
| revolutions per day: | 15.27601153 |
| mean anomaly at epoch: | 92.9743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|