View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43792U 26075.10911691 +.00000000 +00000-0 +14192-3 0 00006
2 43792 97.4107 116.4457 0010218 294.3354 65.6805 15.03945811 02
| Epoch (UTC): | 16 March 2026 02:37:07 |
| Eccentricity: | 0.0010218 |
| inclination: | 97.4107° |
| perigee height: | 548 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 116.4457° |
| argument of perigee: | 294.3354° |
| revolutions per day: | 15.03945811 |
| mean anomaly at epoch: | 65.6805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|