View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48606U 26145.33971463 +.00000000 +00000-0 +21359-3 0 00004
2 48606 52.9939 132.1638 0011576 94.9914 265.2405 15.27193439 01
| Epoch (UTC): | 25 May 2026 08:09:11 |
| Eccentricity: | 0.0011576 |
| inclination: | 52.9939° |
| perigee height: | 476 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 132.1638° |
| argument of perigee: | 94.9914° |
| revolutions per day: | 15.27193439 |
| mean anomaly at epoch: | 265.2405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|