View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68989U 26145.28144779 +.00000000 +00000-0 +17518-3 0 00008
2 68989 97.7419 43.1350 0005332 197.6554 162.4480 14.90766234 02
| Epoch (UTC): | 25 May 2026 06:45:17 |
| Eccentricity: | 0.0005332 |
| inclination: | 97.7419° |
| perigee height: | 592 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 43.1350° |
| argument of perigee: | 197.6554° |
| revolutions per day: | 14.90766234 |
| mean anomaly at epoch: | 162.4480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|