View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64573U 26101.09685794 +.00000000 +00000-0 +10662-3 0 00004
2 64573 97.7126 216.0047 0003059 170.4021 189.7259 14.97149639 05
| Epoch (UTC): | 11 April 2026 02:19:28 |
| Eccentricity: | 0.0003059 |
| inclination: | 97.7126° |
| perigee height: | 574 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 216.0047° |
| argument of perigee: | 170.4021° |
| revolutions per day: | 14.97149639 |
| mean anomaly at epoch: | 189.7259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|