View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40376U 26064.96875367 +.00000000 +00000-0 +13913-3 0 00002
2 40376 98.1312 73.5094 0001294 112.8436 247.2903 14.63332903 06
| Epoch (UTC): | 05 March 2026 23:15:00 |
| Eccentricity: | 0.0001294 |
| inclination: | 98.1312° |
| perigee height: | 682 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 73.5094° |
| argument of perigee: | 112.8436° |
| revolutions per day: | 14.63332903 |
| mean anomaly at epoch: | 247.2903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|