View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18096U 26067.58789993 +.00000000 +00000-0 +11448-3 0 00007
2 18096 74.0413 130.3181 0022560 240.8391 119.0505 14.37955193 02
| Epoch (UTC): | 08 March 2026 14:06:34 |
| Eccentricity: | 0.0022560 |
| inclination: | 74.0413° |
| perigee height: | 749 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 130.3181° |
| argument of perigee: | 240.8391° |
| revolutions per day: | 14.37955193 |
| mean anomaly at epoch: | 119.0505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|