View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65445U 26145.55032399 +.00000000 +00000-0 +37574-3 0 00000
2 65445 97.4484 359.7724 0001713 84.0027 276.1395 15.05661889 04
| Epoch (UTC): | 25 May 2026 13:12:27 |
| Eccentricity: | 0.0001713 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.7724° |
| argument of perigee: | 84.0027° |
| revolutions per day: | 15.05661889 |
| mean anomaly at epoch: | 276.1395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|