View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69006U 26145.25662910 +.00000000 +00000-0 +22432-3 0 00009
2 69006 97.4074 43.4845 0006055 89.5361 270.6568 15.19971119 08
| Epoch (UTC): | 25 May 2026 06:09:32 |
| Eccentricity: | 0.0006055 |
| inclination: | 97.4074° |
| perigee height: | 502 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 43.4845° |
| argument of perigee: | 89.5361° |
| revolutions per day: | 15.19971119 |
| mean anomaly at epoch: | 270.6568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|