View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62112U 26145.60787613 +.00000000 +00000-0 +19940-3 0 00007
2 62112 49.9418 272.0048 0006868 254.9668 105.0522 15.14431971 01
| Epoch (UTC): | 25 May 2026 14:35:20 |
| Eccentricity: | 0.0006868 |
| inclination: | 49.9418° |
| perigee height: | 518 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 272.0048° |
| argument of perigee: | 254.9668° |
| revolutions per day: | 15.14431971 |
| mean anomaly at epoch: | 105.0522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|