View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62531U 26145.37154953 +.00000000 +00000-0 +63215-3 0 00005
2 62531 43.0006 147.0293 0001446 275.7323 84.3364 15.27607615 00
| Epoch (UTC): | 25 May 2026 08:55:01 |
| Eccentricity: | 0.0001446 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 147.0293° |
| argument of perigee: | 275.7323° |
| revolutions per day: | 15.27607615 |
| mean anomaly at epoch: | 84.3364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|