View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68071U 26145.38087744 +.00000000 +00000-0 +75330-4 0 00006
2 68071 53.1579 182.0285 0001145 58.8638 301.2476 15.34368806 06
| Epoch (UTC): | 25 May 2026 09:08:27 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.1579° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 182.0285° |
| argument of perigee: | 58.8638° |
| revolutions per day: | 15.34368806 |
| mean anomaly at epoch: | 301.2476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|