View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64941U 26145.41659002 +.00000000 +00000-0 +29508-3 0 00009
2 64941 97.4497 9.3699 0002279 94.3290 265.8198 15.05657172 07
| Epoch (UTC): | 25 May 2026 09:59:53 |
| Eccentricity: | 0.0002279 |
| inclination: | 97.4497° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.3699° |
| argument of perigee: | 94.3290° |
| revolutions per day: | 15.05657172 |
| mean anomaly at epoch: | 265.8198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|