View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43476U 18047A 26159.06884230 +.00002562 00000-0 +67869-4 0 06
2 43476 88.9926 199.2086 0013276 136.7438 311.4644 15.38200609448401
| Epoch (UTC): | 08 June 2026 01:39:07 |
| Eccentricity: | 0.0013276 |
| inclination: | 88.9926° |
| perigee height: | 442 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 199.2086° |
| argument of perigee: | 136.7438° |
| revolutions per day: | 15.38200609 |
| mean anomaly at epoch: | 311.4644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|