View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54748U 26144.95050172 +.00000000 +00000-0 +40824-3 0 00008
2 54748 35.0060 341.0621 0003272 320.7007 39.3470 15.23139608 08
| Epoch (UTC): | 24 May 2026 22:48:43 |
| Eccentricity: | 0.0003272 |
| inclination: | 35.0060° |
| perigee height: | 494 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 341.0621° |
| argument of perigee: | 320.7007° |
| revolutions per day: | 15.23139608 |
| mean anomaly at epoch: | 39.3470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|