View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40059U 26088.15530183 +.00000000 +00000-0 +16084-3 0 00003
2 40059 98.1955 30.6958 0001517 92.7620 267.3752 14.57116674 02
| Epoch (UTC): | 29 March 2026 03:43:38 |
| Eccentricity: | 0.0001517 |
| inclination: | 98.1955° |
| perigee height: | 701 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 30.6958° |
| argument of perigee: | 92.7620° |
| revolutions per day: | 14.57116674 |
| mean anomaly at epoch: | 267.3752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|