View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63458U 26145.58335647 +.00000000 +00000-0 -45270-4 0 00001
2 63458 53.1582 142.8789 0001359 84.1123 199.0708 15.42157455 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001359 |
| inclination: | 53.1582° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 142.8789° |
| argument of perigee: | 84.1123° |
| revolutions per day: | 15.42157455 |
| mean anomaly at epoch: | 199.0708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|