View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63410U 26145.40735069 +.00000000 +00000-0 +64553-3 0 00005
2 63410 43.0053 33.7475 0001569 271.3286 88.7386 15.27591452 01
| Epoch (UTC): | 25 May 2026 09:46:35 |
| Eccentricity: | 0.0001569 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.7475° |
| argument of perigee: | 271.3286° |
| revolutions per day: | 15.27591452 |
| mean anomaly at epoch: | 88.7386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|