View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63047U 26145.29026678 +.00000000 +00000-0 +66919-3 0 00005
2 63047 53.1597 262.3987 0001285 88.5114 271.6034 15.30210793 06
| Epoch (UTC): | 25 May 2026 06:57:59 |
| Eccentricity: | 0.0001285 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 262.3987° |
| argument of perigee: | 88.5114° |
| revolutions per day: | 15.30210793 |
| mean anomaly at epoch: | 271.6034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|