View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62248U 26145.64378984 +.00000000 +00000-0 +14768-3 0 00001
2 62248 89.0097 24.7435 0016871 83.8404 276.4669 13.51010015 09
| Epoch (UTC): | 25 May 2026 15:27:03 |
| Eccentricity: | 0.0016871 |
| inclination: | 89.0097° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 24.7435° |
| argument of perigee: | 83.8404° |
| revolutions per day: | 13.51010015 |
| mean anomaly at epoch: | 276.4669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|