View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49387U 26145.64863171 +.00000000 +00000-0 +25438-3 0 00003
2 49387 97.2652 193.4336 0008577 24.6053 335.5590 15.19798196 06
| Epoch (UTC): | 25 May 2026 15:34:01 |
| Eccentricity: | 0.0008577 |
| inclination: | 97.2652° |
| perigee height: | 501 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 193.4336° |
| argument of perigee: | 24.6053° |
| revolutions per day: | 15.19798196 |
| mean anomaly at epoch: | 335.5590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|