View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64710U 26145.35479904 +.00000000 +00000-0 +14484-3 0 00004
2 64710 70.0000 121.1525 0003992 264.5313 95.5390 14.98342336 05
| Epoch (UTC): | 25 May 2026 08:30:54 |
| Eccentricity: | 0.0003992 |
| inclination: | 70.0000° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1525° |
| argument of perigee: | 264.5313° |
| revolutions per day: | 14.98342336 |
| mean anomaly at epoch: | 95.5390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|