View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67014U 26145.58157756 +.00000000 +00000-0 +29467-3 0 00004
2 67014 70.0004 260.6548 0003133 268.4625 91.6176 14.98338161 09
| Epoch (UTC): | 25 May 2026 13:57:28 |
| Eccentricity: | 0.0003133 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.6548° |
| argument of perigee: | 268.4625° |
| revolutions per day: | 14.98338161 |
| mean anomaly at epoch: | 91.6176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|