View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67127U 26145.54450477 +.00000000 +00000-0 +60788-3 0 00002
2 67127 42.9983 94.6516 0000481 83.5231 276.5675 15.27582425 05
| Epoch (UTC): | 25 May 2026 13:04:05 |
| Eccentricity: | 0.0000481 |
| inclination: | 42.9983° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 94.6516° |
| argument of perigee: | 83.5231° |
| revolutions per day: | 15.27582425 |
| mean anomaly at epoch: | 276.5675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|