View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00016U 26087.27932528 +.00000000 +00000-0 +32492-4 0 00005
2 00016 34.2581 178.9925 2019413 138.8704 238.3080 10.49580969 09
| Epoch (UTC): | 28 March 2026 06:42:13 |
| Eccentricity: | 0.2019413 |
| inclination: | 34.2581° |
| perigee height: | 654 km |
| apogee height: | 4213 km |
| right ascension of ascending node: | 178.9925° |
| argument of perigee: | 138.8704° |
| revolutions per day: | 10.49580969 |
| mean anomaly at epoch: | 238.3080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|