View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64889U 26145.58710297 +.00000000 +00000-0 +18116-3 0 00005
2 64889 97.4576 113.4640 0005377 252.7243 107.3408 15.26270793 06
| Epoch (UTC): | 25 May 2026 14:05:25 |
| Eccentricity: | 0.0005377 |
| inclination: | 97.4576° |
| perigee height: | 483 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 113.4640° |
| argument of perigee: | 252.7243° |
| revolutions per day: | 15.26270793 |
| mean anomaly at epoch: | 107.3408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|