View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18096U 26069.11846788 +.00000000 +00000-0 +98094-4 0 00007
2 18096 74.0410 127.5004 0022553 237.8665 122.0301 14.37956006 05
| Epoch (UTC): | 10 March 2026 02:50:35 |
| Eccentricity: | 0.0022553 |
| inclination: | 74.0410° |
| perigee height: | 749 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 127.5004° |
| argument of perigee: | 237.8665° |
| revolutions per day: | 14.37956006 |
| mean anomaly at epoch: | 122.0301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|