View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13028U 26074.89324189 +.00000000 +00000-0 +11078-3 0 00000
2 13028 74.0382 261.6533 0020183 274.2536 85.6313 14.39880113 03
| Epoch (UTC): | 15 March 2026 21:26:16 |
| Eccentricity: | 0.0020183 |
| inclination: | 74.0382° |
| perigee height: | 744 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 261.6533° |
| argument of perigee: | 274.2536° |
| revolutions per day: | 14.39880113 |
| mean anomaly at epoch: | 85.6313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|