View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67311U 26145.60065416 +.00000000 +00000-0 +38145-3 0 00001
2 67311 42.9999 250.7266 0001234 279.0308 81.0404 15.27588177 07
| Epoch (UTC): | 25 May 2026 14:24:56 |
| Eccentricity: | 0.0001234 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.7266° |
| argument of perigee: | 279.0308° |
| revolutions per day: | 15.27588177 |
| mean anomaly at epoch: | 81.0404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|