View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42767U 26145.65103394 +.00000000 +00000-0 +18013-3 0 00004
2 42767 97.4282 205.8226 0003637 44.3776 315.7750 15.19274558 00
| Epoch (UTC): | 25 May 2026 15:37:29 |
| Eccentricity: | 0.0003637 |
| inclination: | 97.4282° |
| perigee height: | 506 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 205.8226° |
| argument of perigee: | 44.3776° |
| revolutions per day: | 15.19274558 |
| mean anomaly at epoch: | 315.7750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|