View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64888U 26145.57624900 +.00000000 +00000-0 +77346-3 0 00008
2 64888 97.4461 116.1044 0004270 216.1491 143.9466 15.40214947 01
| Epoch (UTC): | 25 May 2026 13:49:47 |
| Eccentricity: | 0.0004270 |
| inclination: | 97.4461° |
| perigee height: | 443 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 116.1044° |
| argument of perigee: | 216.1491° |
| revolutions per day: | 15.40214947 |
| mean anomaly at epoch: | 143.9466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|