View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65454U 26145.30572700 +.00000000 +00000-0 +19512-3 0 00000
2 65454 97.5144 359.9655 0002218 88.6950 271.4530 15.04839203 04
| Epoch (UTC): | 25 May 2026 07:20:14 |
| Eccentricity: | 0.0002218 |
| inclination: | 97.5144° |
| perigee height: | 550 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 359.9655° |
| argument of perigee: | 88.6950° |
| revolutions per day: | 15.04839203 |
| mean anomaly at epoch: | 271.4530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|