View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61936U 26145.50850756 +.00000000 +00000-0 +74446-4 0 00001
2 61936 98.0033 153.5767 0000685 129.9274 230.1995 14.73311999 03
| Epoch (UTC): | 25 May 2026 12:12:15 |
| Eccentricity: | 0.0000685 |
| inclination: | 98.0033° |
| perigee height: | 650 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 153.5767° |
| argument of perigee: | 129.9274° |
| revolutions per day: | 14.73311999 |
| mean anomaly at epoch: | 230.1995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|