View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14129U 26140.20547571 +.00000000 +00000-0 +00000-0 0 00004
2 14129 25.8960 224.2131 6020565 107.9633 323.3103 2.05872908 03
| Epoch (UTC): | 20 May 2026 04:55:53 |
| Eccentricity: | 0.6020565 |
| inclination: | 25.8960° |
| perigee height: | 4009 km |
| apogee height: | 35438 km |
| right ascension of ascending node: | 224.2131° |
| argument of perigee: | 107.9633° |
| revolutions per day: | 2.05872908 |
| mean anomaly at epoch: | 323.3103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|