View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69014U 26145.24217464 +.00000000 +00000-0 +16225-3 0 00000
2 69014 97.4089 43.5121 0007440 126.9274 233.2645 15.20957819 03
| Epoch (UTC): | 25 May 2026 05:48:43 |
| Eccentricity: | 0.0007440 |
| inclination: | 97.4089° |
| perigee height: | 498 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 43.5121° |
| argument of perigee: | 126.9274° |
| revolutions per day: | 15.20957819 |
| mean anomaly at epoch: | 233.2645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|