View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12443U 26067.50472902 +.00000000 +00000-0 +10566-3 0 00008
2 12443 74.0516 93.5763 0003211 141.0023 219.1362 14.36032395 00
| Epoch (UTC): | 08 March 2026 12:06:48 |
| Eccentricity: | 0.0003211 |
| inclination: | 74.0516° |
| perigee height: | 769 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 93.5763° |
| argument of perigee: | 141.0023° |
| revolutions per day: | 14.36032395 |
| mean anomaly at epoch: | 219.1362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|