View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64187U 26145.23555310 +.00000000 +00000-0 +94190-3 0 00007
2 64187 53.1584 95.6524 0001312 55.8682 304.2443 15.30201454 01
| Epoch (UTC): | 25 May 2026 05:39:11 |
| Eccentricity: | 0.0001312 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.6524° |
| argument of perigee: | 55.8682° |
| revolutions per day: | 15.30201454 |
| mean anomaly at epoch: | 304.2443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|