View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64148U 26145.10429712 +.00000000 +00000-0 +38613-3 0 00004
2 64148 97.4463 196.4250 0002437 108.5519 251.5973 15.05660779 08
| Epoch (UTC): | 25 May 2026 02:30:11 |
| Eccentricity: | 0.0002437 |
| inclination: | 97.4463° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.4250° |
| argument of perigee: | 108.5519° |
| revolutions per day: | 15.05660779 |
| mean anomaly at epoch: | 251.5973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|