View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68148U 26145.52729385 +.00000000 +00000-0 +37953-3 0 00009
2 68148 97.2848 167.1855 0001004 64.9011 295.2336 15.33434291 01
| Epoch (UTC): | 25 May 2026 12:39:18 |
| Eccentricity: | 0.0001004 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.1855° |
| argument of perigee: | 64.9011° |
| revolutions per day: | 15.33434291 |
| mean anomaly at epoch: | 295.2336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|