View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61576U 26145.10628368 +.00000000 +00000-0 +11652-4 0 00009
2 61576 53.1595 279.4555 0000979 96.3369 263.7760 15.69710385 09
| Epoch (UTC): | 25 May 2026 02:33:02 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 279.4555° |
| argument of perigee: | 96.3369° |
| revolutions per day: | 15.69710385 |
| mean anomaly at epoch: | 263.7760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|