View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49732U 26145.50903073 +.00000000 +00000-0 -15046-4 0 00004
2 49732 53.2108 174.4210 0001136 71.3807 288.7308 15.08837748 09
| Epoch (UTC): | 25 May 2026 12:13:00 |
| Eccentricity: | 0.0001136 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 174.4210° |
| argument of perigee: | 71.3807° |
| revolutions per day: | 15.08837748 |
| mean anomaly at epoch: | 288.7308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|