View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19211U 26037.82370928 +.00000000 +00000-0 +79151-4 0 00001
2 19211 82.5273 127.3936 0021830 143.7379 216.5322 14.85351935 07
| Epoch (UTC): | 06 February 2026 19:46:08 |
| Eccentricity: | 0.0021830 |
| inclination: | 82.5273° |
| perigee height: | 597 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 127.3936° |
| argument of perigee: | 143.7379° |
| revolutions per day: | 14.85351935 |
| mean anomaly at epoch: | 216.5322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|