View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00012U 26104.07957615 +.00000000 +00000-0 +11426-3 0 00006
2 00012 32.8963 91.1533 1646271 125.6845 250.8346 11.48595258 02
| Epoch (UTC): | 14 April 2026 01:54:35 |
| Eccentricity: | 0.1646271 |
| inclination: | 32.8963° |
| perigee height: | 554 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 91.1533° |
| argument of perigee: | 125.6845° |
| revolutions per day: | 11.48595258 |
| mean anomaly at epoch: | 250.8346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|