View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67618U 26145.20072662 +.00000000 +00000-0 +62143-3 0 00003
2 67618 43.0000 67.7920 0001413 265.3859 94.6831 15.27590251 03
| Epoch (UTC): | 25 May 2026 04:49:02 |
| Eccentricity: | 0.0001413 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 67.7920° |
| argument of perigee: | 265.3859° |
| revolutions per day: | 15.27590251 |
| mean anomaly at epoch: | 94.6831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|