View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69103U 26145.42220529 +.00000000 +00000-0 +18076-3 0 00001
2 69103 51.6330 52.7989 0007470 96.3597 263.8242 15.49365963 04
| Epoch (UTC): | 25 May 2026 10:07:58 |
| Eccentricity: | 0.0007470 |
| inclination: | 51.6330° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 52.7989° |
| argument of perigee: | 96.3597° |
| revolutions per day: | 15.49365963 |
| mean anomaly at epoch: | 263.8242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|