View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66621U 26145.36784812 +.00000000 +00000-0 +39979-3 0 00001
2 66621 53.1561 143.9606 0001065 96.5337 263.5785 15.30205364 03
| Epoch (UTC): | 25 May 2026 08:49:42 |
| Eccentricity: | 0.0001065 |
| inclination: | 53.1561° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.9606° |
| argument of perigee: | 96.5337° |
| revolutions per day: | 15.30205364 |
| mean anomaly at epoch: | 263.5785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|