View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65489U 26145.09198002 +.00000000 +00000-0 +25826-3 0 00008
2 65489 97.4046 331.8317 0014728 93.9166 266.3753 15.19610688 03
| Epoch (UTC): | 25 May 2026 02:12:27 |
| Eccentricity: | 0.0014728 |
| inclination: | 97.4046° |
| perigee height: | 497 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 331.8317° |
| argument of perigee: | 93.9166° |
| revolutions per day: | 15.19610688 |
| mean anomaly at epoch: | 266.3753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|