View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40554U 26145.65737329 +.00000000 +00000-0 +36153-3 0 00002
2 40554 82.4876 44.7680 0014643 24.3289 335.8479 12.42869485 08
| Epoch (UTC): | 25 May 2026 15:46:37 |
| Eccentricity: | 0.0014643 |
| inclination: | 82.4876° |
| perigee height: | 1483 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 44.7680° |
| argument of perigee: | 24.3289° |
| revolutions per day: | 12.42869485 |
| mean anomaly at epoch: | 335.8479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|