View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37165U 26150.56367992 +.00000000 +00000-0 +13596-3 0 00003
2 37165 98.3877 15.8341 0033605 300.1240 59.6642 14.82053407 01
| Epoch (UTC): | 30 May 2026 13:31:41 |
| Eccentricity: | 0.0033605 |
| inclination: | 98.3877° |
| perigee height: | 599 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 15.8341° |
| argument of perigee: | 300.1240° |
| revolutions per day: | 14.82053407 |
| mean anomaly at epoch: | 59.6642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|