View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 03093U 26106.25226821 +.00000000 +00000-0 +10745-3 0 00001
2 03093 105.7978 333.4013 0319148 206.4545 262.7604 12.83601410 06
| Epoch (UTC): | 16 April 2026 06:03:15 |
| Eccentricity: | 0.0319148 |
| inclination: | 105.7978° |
| perigee height: | 1081 km |
| apogee height: | 1573 km |
| right ascension of ascending node: | 333.4013° |
| argument of perigee: | 206.4545° |
| revolutions per day: | 12.83601410 |
| mean anomaly at epoch: | 262.7604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|