View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64347U 26145.56017834 +.00000000 +00000-0 -58383-4 0 00001
2 64347 70.0008 200.7437 0004111 269.0890 90.9798 14.98330322 02
| Epoch (UTC): | 25 May 2026 13:26:39 |
| Eccentricity: | 0.0004111 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.7437° |
| argument of perigee: | 269.0890° |
| revolutions per day: | 14.98330322 |
| mean anomaly at epoch: | 90.9798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|