View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54005U 26145.50943125 +.00000000 +00000-0 -52046-5 0 00007
2 54005 53.2155 228.9819 0001185 88.0406 272.0722 15.08841502 03
| Epoch (UTC): | 25 May 2026 12:13:34 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 228.9819° |
| argument of perigee: | 88.0406° |
| revolutions per day: | 15.08841502 |
| mean anomaly at epoch: | 272.0722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|