View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18123U 26140.57010733 +.00000000 +00000-0 +26528-4 0 00004
2 18123 98.7334 327.0120 0011510 237.8921 122.1138 14.19548432 05
| Epoch (UTC): | 20 May 2026 13:40:57 |
| Eccentricity: | 0.0011510 |
| inclination: | 98.7334° |
| perigee height: | 819 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 327.0120° |
| argument of perigee: | 237.8921° |
| revolutions per day: | 14.19548432 |
| mean anomaly at epoch: | 122.1138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|