View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61738U 26145.62371411 +.00000000 +00000-0 +21726-3 0 00002
2 61738 97.3244 346.3982 0007590 134.6475 225.5368 14.97474809 06
| Epoch (UTC): | 25 May 2026 14:58:08 |
| Eccentricity: | 0.0007590 |
| inclination: | 97.3244° |
| perigee height: | 569 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 346.3982° |
| argument of perigee: | 134.6475° |
| revolutions per day: | 14.97474809 |
| mean anomaly at epoch: | 225.5368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|