View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64504U 26145.58053111 +.00000000 +00000-0 +46661-3 0 00000
2 64504 51.9001 253.0304 0000252 119.1161 240.9827 14.79942452 02
| Epoch (UTC): | 25 May 2026 13:55:57 |
| Eccentricity: | 0.0000252 |
| inclination: | 51.9001° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 253.0304° |
| argument of perigee: | 119.1161° |
| revolutions per day: | 14.79942452 |
| mean anomaly at epoch: | 240.9827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|