View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64268U 26145.34471181 +.00000000 +00000-0 +92174-3 0 00002
2 64268 53.1589 118.4169 0001178 87.2718 272.8420 15.34402746 00
| Epoch (UTC): | 25 May 2026 08:16:23 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 118.4169° |
| argument of perigee: | 87.2718° |
| revolutions per day: | 15.34402746 |
| mean anomaly at epoch: | 272.8420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|