View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11870U 26076.11898003 +.00000000 +00000-0 +73826-4 0 00001
2 11870 74.0507 96.4416 0016655 329.4469 30.5714 14.38390586 09
| Epoch (UTC): | 17 March 2026 02:51:19 |
| Eccentricity: | 0.0016655 |
| inclination: | 74.0507° |
| perigee height: | 752 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 96.4416° |
| argument of perigee: | 329.4469° |
| revolutions per day: | 14.38390586 |
| mean anomaly at epoch: | 30.5714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|