View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61893U 26145.24807065 +.00000000 +00000-0 -45030-5 0 00008
2 61893 53.1591 130.4377 0000944 88.1743 271.9368 15.34402875 01
| Epoch (UTC): | 25 May 2026 05:57:13 |
| Eccentricity: | 0.0000944 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.4377° |
| argument of perigee: | 88.1743° |
| revolutions per day: | 15.34402875 |
| mean anomaly at epoch: | 271.9368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|