View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64116U 26145.39713176 +.00000000 +00000-0 +39750-3 0 00003
2 64116 53.1602 29.9738 0001153 93.9732 266.1401 15.31721180 07
| Epoch (UTC): | 25 May 2026 09:31:52 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 29.9738° |
| argument of perigee: | 93.9732° |
| revolutions per day: | 15.31721180 |
| mean anomaly at epoch: | 266.1401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|