View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25407U 26020.96640395 +.00000000 +00000-0 +21354-3 0 00001
2 25407 71.0114 281.9355 0005234 102.5777 257.5932 14.16183982 06
| Epoch (UTC): | 20 January 2026 23:11:37 |
| Eccentricity: | 0.0005234 |
| inclination: | 71.0114° |
| perigee height: | 835 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 281.9355° |
| argument of perigee: | 102.5777° |
| revolutions per day: | 14.16183982 |
| mean anomaly at epoch: | 257.5932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|