View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14148U 26073.26554321 +.00000000 +00000-0 +56449-4 0 00009
2 14148 82.5206 157.0316 0019401 239.6989 120.2309 14.85673926 05
| Epoch (UTC): | 14 March 2026 06:22:22 |
| Eccentricity: | 0.0019401 |
| inclination: | 82.5206° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 157.0316° |
| argument of perigee: | 239.6989° |
| revolutions per day: | 14.85673926 |
| mean anomaly at epoch: | 120.2309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|