View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17192U 26072.22917691 +.00000000 +00000-0 +53153-4 0 00008
2 17192 82.5069 138.8255 0016545 18.7395 38.5042 14.85917746 02
| Epoch (UTC): | 13 March 2026 05:30:00 |
| Eccentricity: | 0.0016545 |
| inclination: | 82.5069° |
| perigee height: | 599 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 138.8255° |
| argument of perigee: | 18.7395° |
| revolutions per day: | 14.85917746 |
| mean anomaly at epoch: | 38.5042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|