View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67363U 26145.00542265 +.00000000 +00000-0 +40904-3 0 00000
2 67363 97.8015 143.9241 0007834 205.9096 154.1729 14.88127296 01
| Epoch (UTC): | 25 May 2026 00:07:48 |
| Eccentricity: | 0.0007834 |
| inclination: | 97.8015° |
| perigee height: | 598 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 143.9241° |
| argument of perigee: | 205.9096° |
| revolutions per day: | 14.88127296 |
| mean anomaly at epoch: | 154.1729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|