View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43187U 26103.73654649 +.00000000 +00000-0 +16008-3 0 00000
2 43187 97.5415 8.9292 0007501 230.0425 130.0149 15.16048910 08
| Epoch (UTC): | 13 April 2026 17:40:37 |
| Eccentricity: | 0.0007501 |
| inclination: | 97.5415° |
| perigee height: | 513 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 8.9292° |
| argument of perigee: | 230.0425° |
| revolutions per day: | 15.16048910 |
| mean anomaly at epoch: | 130.0149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|