View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25338U 26075.85006306 +.00000000 +00000-0 +78374-4 0 00005
2 25338 98.5155 98.9442 0009116 256.4169 103.5997 14.27115573 02
| Epoch (UTC): | 16 March 2026 20:24:05 |
| Eccentricity: | 0.0009116 |
| inclination: | 98.5155° |
| perigee height: | 795 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 98.9442° |
| argument of perigee: | 256.4169° |
| revolutions per day: | 14.27115573 |
| mean anomaly at epoch: | 103.5997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|