View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67053U 26145.55832530 +.00000000 +00000-0 +65895-3 0 00009
2 67053 43.0014 324.1016 0001733 266.4321 93.6333 15.27590787 08
| Epoch (UTC): | 25 May 2026 13:23:59 |
| Eccentricity: | 0.0001733 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.1016° |
| argument of perigee: | 266.4321° |
| revolutions per day: | 15.27590787 |
| mean anomaly at epoch: | 93.6333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|