View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38340U 26038.88568075 +.00000000 +00000-0 +53821-3 0 00009
2 38340 98.1970 166.7776 0007529 241.2596 118.7864 14.90073735 00
| Epoch (UTC): | 07 February 2026 21:15:22 |
| Eccentricity: | 0.0007529 |
| inclination: | 98.1970° |
| perigee height: | 592 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 166.7776° |
| argument of perigee: | 241.2596° |
| revolutions per day: | 14.90073735 |
| mean anomaly at epoch: | 118.7864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|