View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67081U 26145.41792612 +.00000000 +00000-0 +37498-3 0 00009
2 67081 70.0016 180.8743 0004384 262.8007 97.2653 14.98339368 09
| Epoch (UTC): | 25 May 2026 10:01:48 |
| Eccentricity: | 0.0004384 |
| inclination: | 70.0016° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.8743° |
| argument of perigee: | 262.8007° |
| revolutions per day: | 14.98339368 |
| mean anomaly at epoch: | 97.2653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|