View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63053U 26145.06085169 +.00000000 +00000-0 +15801-2 0 00000
2 63053 42.9997 274.8615 0002296 51.0927 309.0145 15.70888869 07
| Epoch (UTC): | 25 May 2026 01:27:37 |
| Eccentricity: | 0.0002296 |
| inclination: | 42.9997° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 274.8615° |
| argument of perigee: | 51.0927° |
| revolutions per day: | 15.70888869 |
| mean anomaly at epoch: | 309.0145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|