View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55926U 26145.23955345 +.00000000 +00000-0 +19253-4 0 00008
2 55926 69.9997 91.5698 0003059 269.1112 90.9696 14.98332497 04
| Epoch (UTC): | 25 May 2026 05:44:57 |
| Eccentricity: | 0.0003059 |
| inclination: | 69.9997° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.5698° |
| argument of perigee: | 269.1112° |
| revolutions per day: | 14.98332497 |
| mean anomaly at epoch: | 90.9696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|