View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68412U 26145.50550052 +.00000000 +00000-0 +44697-4 0 00008
2 68412 84.9671 242.1702 0024470 336.9520 23.0603 14.88385186 07
| Epoch (UTC): | 25 May 2026 12:07:55 |
| Eccentricity: | 0.0024470 |
| inclination: | 84.9671° |
| perigee height: | 586 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 242.1702° |
| argument of perigee: | 336.9520° |
| revolutions per day: | 14.88385186 |
| mean anomaly at epoch: | 23.0603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|