View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25397U 26106.74199182 +.00000000 +00000-0 +30711-4 0 00001
2 25397 99.0059 97.9572 0002085 58.5198 301.6183 14.24416052 01
| Epoch (UTC): | 16 April 2026 17:48:28 |
| Eccentricity: | 0.0002085 |
| inclination: | 99.0059° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 97.9572° |
| argument of perigee: | 58.5198° |
| revolutions per day: | 14.24416052 |
| mean anomaly at epoch: | 301.6183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|