View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67499U 26145.60206856 +.00000000 +00000-0 +34366-3 0 00004
2 67499 43.0011 240.1399 0001353 266.4745 93.5952 15.27589134 08
| Epoch (UTC): | 25 May 2026 14:26:58 |
| Eccentricity: | 0.0001353 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.1399° |
| argument of perigee: | 266.4745° |
| revolutions per day: | 15.27589134 |
| mean anomaly at epoch: | 93.5952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|