View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64043U 26145.41908159 +.00000000 +00000-0 +11772-2 0 00005
2 64043 70.0009 281.0634 0002533 274.5281 85.5588 14.98349534 00
| Epoch (UTC): | 25 May 2026 10:03:28 |
| Eccentricity: | 0.0002533 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.0634° |
| argument of perigee: | 274.5281° |
| revolutions per day: | 14.98349534 |
| mean anomaly at epoch: | 85.5588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|