View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14129U 26084.35916295 +.00000000 +00000-0 +00000-0 0 00000
2 14129 25.9114 233.6020 6040998 92.4738 333.4977 2.05874335 09
| Epoch (UTC): | 25 March 2026 08:37:11 |
| Eccentricity: | 0.6040998 |
| inclination: | 25.9114° |
| perigee height: | 3955 km |
| apogee height: | 35491 km |
| right ascension of ascending node: | 233.6020° |
| argument of perigee: | 92.4738° |
| revolutions per day: | 2.05874335 |
| mean anomaly at epoch: | 333.4977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|