View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32953U 26139.77018757 +.00000000 +00000-0 +24014-3 0 00002
2 32953 82.5064 13.1185 0020090 16.1574 344.0142 12.43178291 09
| Epoch (UTC): | 19 May 2026 18:29:04 |
| Eccentricity: | 0.0020090 |
| inclination: | 82.5064° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 13.1185° |
| argument of perigee: | 16.1574° |
| revolutions per day: | 12.43178291 |
| mean anomaly at epoch: | 344.0142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|