View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62102U 26145.46182192 +.00000000 +00000-0 +50988-3 0 00008
2 62102 42.9984 131.8755 0000893 264.7882 95.2868 15.27591824 08
| Epoch (UTC): | 25 May 2026 11:05:01 |
| Eccentricity: | 0.0000893 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.8755° |
| argument of perigee: | 264.7882° |
| revolutions per day: | 15.27591824 |
| mean anomaly at epoch: | 95.2868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|