View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25338U 26032.45085698 +.00000000 +00000-0 +86596-4 0 00000
2 25338 98.5189 56.6754 0010758 31.1850 328.9968 14.27096841 02
| Epoch (UTC): | 01 February 2026 10:49:14 |
| Eccentricity: | 0.0010758 |
| inclination: | 98.5189° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 56.6754° |
| argument of perigee: | 31.1850° |
| revolutions per day: | 14.27096841 |
| mean anomaly at epoch: | 328.9968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|