View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17192U 26073.58661912 +.00000000 +00000-0 +54569-4 0 00002
2 17192 82.5066 137.5468 0016445 14.3525 99.7750 14.85919184 00
| Epoch (UTC): | 14 March 2026 14:04:43 |
| Eccentricity: | 0.0016445 |
| inclination: | 82.5066° |
| perigee height: | 599 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 137.5468° |
| argument of perigee: | 14.3525° |
| revolutions per day: | 14.85919184 |
| mean anomaly at epoch: | 99.7750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|