View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54170U 26145.37423781 +.00000000 +00000-0 +14652-3 0 00004
2 54170 53.2154 19.9219 0001425 85.5089 274.6066 15.08851300 09
| Epoch (UTC): | 25 May 2026 08:58:54 |
| Eccentricity: | 0.0001425 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 19.9219° |
| argument of perigee: | 85.5089° |
| revolutions per day: | 15.08851300 |
| mean anomaly at epoch: | 274.6066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|