View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18187U 26066.97417846 +.00000000 +00000-0 +35661-4 0 00009
2 18187 65.0115 311.5098 0014470 278.5348 81.4097 14.31502771 05
| Epoch (UTC): | 07 March 2026 23:22:49 |
| Eccentricity: | 0.0014470 |
| inclination: | 65.0115° |
| perigee height: | 776 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 311.5098° |
| argument of perigee: | 278.5348° |
| revolutions per day: | 14.31502771 |
| mean anomaly at epoch: | 81.4097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|