View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25397U 98043D 22178.47824328 .00000008 00000-0 23267-4 0 9990
2 25397 98.8185 128.9731 0002402 82.8997 277.2454 14.23759031244858
| Epoch (UTC): | 27 June 2022 11:28:40 |
| Eccentricity: | 0.0002402 |
| inclination: | 98.8185° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 128.9731° |
| argument of perigee: | 82.8997° |
| revolutions per day: | 14.23759031 |
| mean anomaly at epoch: | 277.2454° |
| orbit number at epoch: | 24485 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|