View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60940U 26145.26463130 +.00000000 +00000-0 +16111-4 0 00009
2 60940 53.1592 134.0700 0000672 56.3341 303.7724 15.30193896 09
| Epoch (UTC): | 25 May 2026 06:21:04 |
| Eccentricity: | 0.0000672 |
| inclination: | 53.1592° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 134.0700° |
| argument of perigee: | 56.3341° |
| revolutions per day: | 15.30193896 |
| mean anomaly at epoch: | 303.7724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|