View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64779U 26145.27207565 +.00000000 +00000-0 +62947-3 0 00009
2 64779 53.1602 246.5486 0001552 88.8102 271.3079 15.34410180 03
| Epoch (UTC): | 25 May 2026 06:31:47 |
| Eccentricity: | 0.0001552 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 246.5486° |
| argument of perigee: | 88.8102° |
| revolutions per day: | 15.34410180 |
| mean anomaly at epoch: | 271.3079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|