View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68662U 26145.35722404 +.00000000 +00000-0 +34305-3 0 00004
2 68662 97.2858 16.8701 0002043 88.8186 271.3290 15.33430066 05
| Epoch (UTC): | 25 May 2026 08:34:24 |
| Eccentricity: | 0.0002043 |
| inclination: | 97.2858° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.8701° |
| argument of perigee: | 88.8186° |
| revolutions per day: | 15.33430066 |
| mean anomaly at epoch: | 271.3290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|