View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40404U 26017.31326712 +.00000000 +00000-0 +21101-3 0 00004
2 40404 98.7960 34.6359 0005407 206.1646 153.9257 14.18777298 00
| Epoch (UTC): | 17 January 2026 07:31:06 |
| Eccentricity: | 0.0005407 |
| inclination: | 98.7960° |
| perigee height: | 826 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 34.6359° |
| argument of perigee: | 206.1646° |
| revolutions per day: | 14.18777298 |
| mean anomaly at epoch: | 153.9257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|