View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64191U 26145.12075097 +.00000000 +00000-0 +91696-3 0 00007
2 64191 53.1597 96.3536 0001241 84.9845 275.1297 15.30205985 02
| Epoch (UTC): | 25 May 2026 02:53:52 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 96.3536° |
| argument of perigee: | 84.9845° |
| revolutions per day: | 15.30205985 |
| mean anomaly at epoch: | 275.1297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|