View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64132U 26145.61430127 +.00000000 +00000-0 +16743-2 0 00004
2 64132 43.0018 230.5001 0001737 271.8948 88.1720 15.70868801 02
| Epoch (UTC): | 25 May 2026 14:44:35 |
| Eccentricity: | 0.0001737 |
| inclination: | 43.0018° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 230.5001° |
| argument of perigee: | 271.8948° |
| revolutions per day: | 15.70868801 |
| mean anomaly at epoch: | 88.1720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|