View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68663U 26145.35179529 +.00000000 +00000-0 +83163-3 0 00005
2 68663 97.2855 16.8801 0001933 94.0730 266.0734 15.33453609 07
| Epoch (UTC): | 25 May 2026 08:26:35 |
| Eccentricity: | 0.0001933 |
| inclination: | 97.2855° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.8801° |
| argument of perigee: | 94.0730° |
| revolutions per day: | 15.33453609 |
| mean anomaly at epoch: | 266.0734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|