View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64378U 26144.91714274 +.00000000 +00000-0 +13832-2 0 00002
2 64378 43.0000 344.8233 0001943 264.9841 95.0805 15.70884708 00
| Epoch (UTC): | 24 May 2026 22:00:41 |
| Eccentricity: | 0.0001943 |
| inclination: | 43.0000° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 344.8233° |
| argument of perigee: | 264.9841° |
| revolutions per day: | 15.70884708 |
| mean anomaly at epoch: | 95.0805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|