View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18187U 26071.72476343 +.00000000 +00000-0 +27854-4 0 00000
2 18187 65.0108 298.2061 0014533 278.8556 81.0883 14.31503616 00
| Epoch (UTC): | 12 March 2026 17:23:39 |
| Eccentricity: | 0.0014533 |
| inclination: | 65.0108° |
| perigee height: | 776 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 298.2061° |
| argument of perigee: | 278.8556° |
| revolutions per day: | 14.31503616 |
| mean anomaly at epoch: | 81.0883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|