View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37818U 26135.08785303 +.00000000 +00000-0 +53312-3 0 00008
2 37818 62.8259 142.4533 4624701 282.7493 30.9538 6.15415056 03
| Epoch (UTC): | 15 May 2026 02:06:30 |
| Eccentricity: | 0.4624701 |
| inclination: | 62.8259° |
| perigee height: | 383 km |
| apogee height: | 12017 km |
| right ascension of ascending node: | 142.4533° |
| argument of perigee: | 282.7493° |
| revolutions per day: | 6.15415056 |
| mean anomaly at epoch: | 30.9538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|