View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67476U 26145.46952119 +.00000000 +00000-0 +75808-4 0 00000
2 67476 44.9805 182.8176 0013079 223.8150 136.1646 13.99159475 06
| Epoch (UTC): | 25 May 2026 11:16:06 |
| Eccentricity: | 0.0013079 |
| inclination: | 44.9805° |
| perigee height: | 887 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 182.8176° |
| argument of perigee: | 223.8150° |
| revolutions per day: | 13.99159475 |
| mean anomaly at epoch: | 136.1646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|