View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67207U 26145.26556142 +.00000000 +00000-0 +17143-3 0 00003
2 67207 70.0014 341.4333 0002537 265.8003 94.2866 14.98334696 06
| Epoch (UTC): | 25 May 2026 06:22:24 |
| Eccentricity: | 0.0002537 |
| inclination: | 70.0014° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.4333° |
| argument of perigee: | 265.8003° |
| revolutions per day: | 14.98334696 |
| mean anomaly at epoch: | 94.2866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|