View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07318U 26106.87431198 +.00000000 +00000-0 +00000-0 0 00008
2 07318 2.0942 249.9580 0029335 346.8057 313.4620 1.01978292 08
| Epoch (UTC): | 16 April 2026 20:59:00 |
| Eccentricity: | 0.0029335 |
| inclination: | 2.0942° |
| perigee height: | 35193 km |
| apogee height: | 35437 km |
| right ascension of ascending node: | 249.9580° |
| argument of perigee: | 346.8057° |
| revolutions per day: | 1.01978292 |
| mean anomaly at epoch: | 313.4620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|