View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48556U 26145.29054997 +.00000000 +00000-0 +12416-3 0 00001
2 48556 53.1594 146.1699 0001050 87.5198 272.5924 15.31728804 07
| Epoch (UTC): | 25 May 2026 06:58:23 |
| Eccentricity: | 0.0001050 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 146.1699° |
| argument of perigee: | 87.5198° |
| revolutions per day: | 15.31728804 |
| mean anomaly at epoch: | 272.5924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|