View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23705U 26039.02301382 +.00000000 +00000-0 +18029-3 0 00002
2 23705 71.0189 242.5393 0012293 174.6585 185.4671 14.15492075 06
| Epoch (UTC): | 08 February 2026 00:33:08 |
| Eccentricity: | 0.0012293 |
| inclination: | 71.0189° |
| perigee height: | 832 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 242.5393° |
| argument of perigee: | 174.6585° |
| revolutions per day: | 14.15492075 |
| mean anomaly at epoch: | 185.4671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|