View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68628U 26145.29767704 +.00000000 +00000-0 +37472-3 0 00009
2 68628 60.0224 266.1651 0021963 359.6187 0.4872 15.23909588 04
| Epoch (UTC): | 25 May 2026 07:08:39 |
| Eccentricity: | 0.0021963 |
| inclination: | 60.0224° |
| perigee height: | 479 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 266.1651° |
| argument of perigee: | 359.6187° |
| revolutions per day: | 15.23909588 |
| mean anomaly at epoch: | 0.4872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|