View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63924U 26145.75431838 +.00000000 +00000-0 +00000-0 0 00004
2 63924 3.3235 317.1005 0001551 253.0037 86.0433 1.00275832 03
| Epoch (UTC): | 25 May 2026 18:06:13 |
| Eccentricity: | 0.0001551 |
| inclination: | 3.3235° |
| perigee height: | 35779 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 317.1005° |
| argument of perigee: | 253.0037° |
| revolutions per day: | 1.00275832 |
| mean anomaly at epoch: | 86.0433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|