View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37372U 26154.54450659 +.00000000 +00000-0 +00000-0 0 00001
2 37372 65.4160 314.9485 0008183 329.8476 359.2972 2.12911563 06
| Epoch (UTC): | 03 June 2026 13:04:05 |
| Eccentricity: | 0.0008183 |
| inclination: | 65.4160° |
| perigee height: | 19124 km |
| apogee height: | 19166 km |
| right ascension of ascending node: | 314.9485° |
| argument of perigee: | 329.8476° |
| revolutions per day: | 2.12911563 |
| mean anomaly at epoch: | 359.2972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|