View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64704U 26145.33810588 +.00000000 +00000-0 +27552-3 0 00002
2 64704 70.0000 121.1336 0003729 264.8053 95.2680 14.98336344 01
| Epoch (UTC): | 25 May 2026 08:06:52 |
| Eccentricity: | 0.0003729 |
| inclination: | 70.0000° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1336° |
| argument of perigee: | 264.8053° |
| revolutions per day: | 14.98336344 |
| mean anomaly at epoch: | 95.2680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|