View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37869U 26145.50049434 +.00000000 +00000-0 +00000-0 0 00003
2 37869 65.2718 73.7371 0026346 254.7192 280.9848 2.13101611 08
| Epoch (UTC): | 25 May 2026 12:00:42 |
| Eccentricity: | 0.0026346 |
| inclination: | 65.2718° |
| perigee height: | 19063 km |
| apogee height: | 19197 km |
| right ascension of ascending node: | 73.7371° |
| argument of perigee: | 254.7192° |
| revolutions per day: | 2.13101611 |
| mean anomaly at epoch: | 280.9848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|