View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64542U 26145.35742639 +.00000000 +00000-0 +36747-3 0 00001
2 64542 97.4672 261.5602 0001597 231.3268 128.7827 15.25420127 01
| Epoch (UTC): | 25 May 2026 08:34:41 |
| Eccentricity: | 0.0001597 |
| inclination: | 97.4672° |
| perigee height: | 488 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 261.5602° |
| argument of perigee: | 231.3268° |
| revolutions per day: | 15.25420127 |
| mean anomaly at epoch: | 128.7827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|