View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10820U 26067.51519369 +.00000000 +00000-0 +23803-3 0 00003
2 10820 98.4533 263.9904 0008267 291.1724 68.8580 14.37987512 09
| Epoch (UTC): | 08 March 2026 12:21:52 |
| Eccentricity: | 0.0008267 |
| inclination: | 98.4533° |
| perigee height: | 759 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 263.9904° |
| argument of perigee: | 291.1724° |
| revolutions per day: | 14.37987512 |
| mean anomaly at epoch: | 68.8580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|