View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21903U 26067.90311365 +.00000000 +00000-0 +67536-4 0 00008
2 21903 82.9413 342.8531 0041872 208.5255 223.0362 13.74743668 06
| Epoch (UTC): | 08 March 2026 21:40:29 |
| Eccentricity: | 0.0041872 |
| inclination: | 82.9413° |
| perigee height: | 952 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 342.8531° |
| argument of perigee: | 208.5255° |
| revolutions per day: | 13.74743668 |
| mean anomaly at epoch: | 223.0362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|