View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67838U 26145.52590470 +.00000000 +00000-0 +24739-3 0 00003
2 67838 43.0016 193.2465 0000916 292.4917 67.5838 15.27576903 00
| Epoch (UTC): | 25 May 2026 12:37:18 |
| Eccentricity: | 0.0000916 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.2465° |
| argument of perigee: | 292.4917° |
| revolutions per day: | 15.27576903 |
| mean anomaly at epoch: | 67.5838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|