View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64249U 26145.59778000 +.00000000 +00000-0 +74307-3 0 00006
2 64249 42.9995 232.5174 0001457 272.7080 87.3605 15.27602777 05
| Epoch (UTC): | 25 May 2026 14:20:48 |
| Eccentricity: | 0.0001457 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 232.5174° |
| argument of perigee: | 272.7080° |
| revolutions per day: | 15.27602777 |
| mean anomaly at epoch: | 87.3605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|