View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00050U 26049.28299102 +.00000000 +00000-0 -16602-4 0 00002
2 00050 47.2292 170.7989 0112999 20.6247 339.9054 12.20162793 02
| Epoch (UTC): | 18 February 2026 06:47:30 |
| Eccentricity: | 0.0112999 |
| inclination: | 47.2292° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 170.7989° |
| argument of perigee: | 20.6247° |
| revolutions per day: | 12.20162793 |
| mean anomaly at epoch: | 339.9054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|