View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37841U 26129.47566784 +.00000000 +00000-0 +69174-4 0 00004
2 37841 19.9729 293.7862 0011752 137.8638 248.7184 14.11567103 04
| Epoch (UTC): | 09 May 2026 11:24:57 |
| Eccentricity: | 0.0011752 |
| inclination: | 19.9729° |
| perigee height: | 846 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 293.7862° |
| argument of perigee: | 137.8638° |
| revolutions per day: | 14.11567103 |
| mean anomaly at epoch: | 248.7184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|