View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38338U 26145.58730419 +.00000000 +00000-0 +80470-4 0 00006
2 38338 98.1160 103.4397 0005341 170.7971 189.3330 14.62182603 04
| Epoch (UTC): | 25 May 2026 14:05:43 |
| Eccentricity: | 0.0005341 |
| inclination: | 98.1160° |
| perigee height: | 682 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 103.4397° |
| argument of perigee: | 170.7971° |
| revolutions per day: | 14.62182603 |
| mean anomaly at epoch: | 189.3330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|