View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64235U 26145.30499601 +.00000000 +00000-0 +13942-2 0 00004
2 64235 43.0009 107.3641 0001706 255.9228 104.1450 15.70882313 00
| Epoch (UTC): | 25 May 2026 07:19:11 |
| Eccentricity: | 0.0001706 |
| inclination: | 43.0009° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 107.3641° |
| argument of perigee: | 255.9228° |
| revolutions per day: | 15.70882313 |
| mean anomaly at epoch: | 104.1450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|