View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53045U 26145.49116524 +.00000000 +00000-0 +80456-3 0 00006
2 53045 97.4468 326.5289 0001599 105.0452 255.0952 15.05594986 03
| Epoch (UTC): | 25 May 2026 11:47:16 |
| Eccentricity: | 0.0001599 |
| inclination: | 97.4468° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.5289° |
| argument of perigee: | 105.0452° |
| revolutions per day: | 15.05594986 |
| mean anomaly at epoch: | 255.0952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|