View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55164U 26145.38916933 +.00000000 +00000-0 -36407-3 0 00008
2 55164 87.9149 10.4134 0002519 92.8140 267.3280 13.17649002 06
| Epoch (UTC): | 25 May 2026 09:20:24 |
| Eccentricity: | 0.0002519 |
| inclination: | 87.9149° |
| perigee height: | 1192 km |
| apogee height: | 1196 km |
| right ascension of ascending node: | 10.4134° |
| argument of perigee: | 92.8140° |
| revolutions per day: | 13.17649002 |
| mean anomaly at epoch: | 267.3280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|