View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37930U 26145.59862303 +.00000000 +00000-0 +97535-4 0 00002
2 37930 98.6995 163.1860 0014844 178.2105 334.4160 14.30533202 04
| Epoch (UTC): | 25 May 2026 14:22:01 |
| Eccentricity: | 0.0014844 |
| inclination: | 98.6995° |
| perigee height: | 779 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 163.1860° |
| argument of perigee: | 178.2105° |
| revolutions per day: | 14.30533202 |
| mean anomaly at epoch: | 334.4160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|