View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19650U 26037.89615352 +.00000000 +00000-0 +83808-4 0 00002
2 19650 70.9970 216.2855 0012336 52.4484 307.7758 14.16146384 01
| Epoch (UTC): | 06 February 2026 21:30:27 |
| Eccentricity: | 0.0012336 |
| inclination: | 70.9970° |
| perigee height: | 830 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 216.2855° |
| argument of perigee: | 52.4484° |
| revolutions per day: | 14.16146384 |
| mean anomaly at epoch: | 307.7758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|