View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43437U 26145.60788416 +.00000000 +00000-0 +43115-4 0 00000
2 43437 98.6253 213.4630 0001180 74.4441 285.6869 14.26734178 06
| Epoch (UTC): | 25 May 2026 14:35:21 |
| Eccentricity: | 0.0001180 |
| inclination: | 98.6253° |
| perigee height: | 802 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 213.4630° |
| argument of perigee: | 74.4441° |
| revolutions per day: | 14.26734178 |
| mean anomaly at epoch: | 285.6869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|