View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43812U 26145.05875803 +.00000000 +00000-0 +20099-3 0 00008
2 43812 97.3571 182.5348 0004789 221.2703 138.8165 15.08511144 00
| Epoch (UTC): | 25 May 2026 01:24:36 |
| Eccentricity: | 0.0004789 |
| inclination: | 97.3571° |
| perigee height: | 537 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 182.5348° |
| argument of perigee: | 221.2703° |
| revolutions per day: | 15.08511144 |
| mean anomaly at epoch: | 138.8165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|