View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62786U 26145.47236530 +.00000000 +00000-0 +12996-3 0 00000
2 62786 88.9708 86.0224 0013773 234.4903 125.4964 13.51014131 00
| Epoch (UTC): | 25 May 2026 11:20:12 |
| Eccentricity: | 0.0013773 |
| inclination: | 88.9708° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 86.0224° |
| argument of perigee: | 234.4903° |
| revolutions per day: | 13.51014131 |
| mean anomaly at epoch: | 125.4964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|