View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44777U 26145.57319209 +.00000000 +00000-0 +37153-3 0 00008
2 44777 97.4964 228.8465 0007309 153.9560 206.2054 15.38609170 02
| Epoch (UTC): | 25 May 2026 13:45:23 |
| Eccentricity: | 0.0007309 |
| inclination: | 97.4964° |
| perigee height: | 445 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 228.8465° |
| argument of perigee: | 153.9560° |
| revolutions per day: | 15.38609170 |
| mean anomaly at epoch: | 206.2054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|