View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19210U 26075.17183516 +.00000000 +00000-0 +26127-3 0 00009
2 19210 82.5102 151.7282 0012646 102.1084 258.1573 15.28641799 07
| Epoch (UTC): | 16 March 2026 04:07:26 |
| Eccentricity: | 0.0012646 |
| inclination: | 82.5102° |
| perigee height: | 471 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 151.7282° |
| argument of perigee: | 102.1084° |
| revolutions per day: | 15.28641799 |
| mean anomaly at epoch: | 258.1573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|