View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49003U 26145.64115669 +.00000000 +00000-0 +30123-3 0 00007
2 49003 97.5203 222.2515 0008668 139.0252 221.1631 15.09879647 05
| Epoch (UTC): | 25 May 2026 15:23:15 |
| Eccentricity: | 0.0008668 |
| inclination: | 97.5203° |
| perigee height: | 531 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 222.2515° |
| argument of perigee: | 139.0252° |
| revolutions per day: | 15.09879647 |
| mean anomaly at epoch: | 221.1631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|