View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68153U 26145.07326532 +.00000000 +00000-0 +14497-2 0 00009
2 68153 97.2852 166.7380 0000959 145.2859 214.8446 15.33436542 01
| Epoch (UTC): | 25 May 2026 01:45:30 |
| Eccentricity: | 0.0000959 |
| inclination: | 97.2852° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.7380° |
| argument of perigee: | 145.2859° |
| revolutions per day: | 15.33436542 |
| mean anomaly at epoch: | 214.8446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|