View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65670U 26145.36813058 +.00000000 +00000-0 +42680-3 0 00002
2 65670 97.4462 189.3356 0002255 131.6157 228.5264 15.05656655 04
| Epoch (UTC): | 25 May 2026 08:50:06 |
| Eccentricity: | 0.0002255 |
| inclination: | 97.4462° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.3356° |
| argument of perigee: | 131.6157° |
| revolutions per day: | 15.05656655 |
| mean anomaly at epoch: | 228.5264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|