View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40376U 26072.96893316 +.00000000 +00000-0 +12970-3 0 00007
2 40376 98.1311 81.3977 0001530 110.0399 250.0968 14.63345282 00
| Epoch (UTC): | 13 March 2026 23:15:15 |
| Eccentricity: | 0.0001530 |
| inclination: | 98.1311° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 81.3977° |
| argument of perigee: | 110.0399° |
| revolutions per day: | 14.63345282 |
| mean anomaly at epoch: | 250.0968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|