View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65556U 26145.26756667 +.00000000 +00000-0 +18655-3 0 00001
2 65556 49.9870 145.4514 0013566 226.4701 133.5112 14.84102071 07
| Epoch (UTC): | 25 May 2026 06:25:17 |
| Eccentricity: | 0.0013566 |
| inclination: | 49.9870° |
| perigee height: | 607 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 145.4514° |
| argument of perigee: | 226.4701° |
| revolutions per day: | 14.84102071 |
| mean anomaly at epoch: | 133.5112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|