View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66675U 26145.13944071 +.00000000 +00000-0 +39934-3 0 00001
2 66675 97.4180 219.0605 0007450 90.2988 269.9101 15.20375705 09
| Epoch (UTC): | 25 May 2026 03:20:47 |
| Eccentricity: | 0.0007450 |
| inclination: | 97.4180° |
| perigee height: | 500 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 219.0605° |
| argument of perigee: | 90.2988° |
| revolutions per day: | 15.20375705 |
| mean anomaly at epoch: | 269.9101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|