View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63508U 26145.38253880 +.00000000 +00000-0 +42127-3 0 00009
2 63508 53.1595 143.5331 0001094 85.2584 274.8542 15.30208121 03
| Epoch (UTC): | 25 May 2026 09:10:51 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.5331° |
| argument of perigee: | 85.2584° |
| revolutions per day: | 15.30208121 |
| mean anomaly at epoch: | 274.8542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|