View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60277U 26145.45714198 +.00000000 +00000-0 +10609-5 0 00003
2 60277 53.1602 55.7349 0001100 98.8136 261.2990 15.30190356 03
| Epoch (UTC): | 25 May 2026 10:58:17 |
| Eccentricity: | 0.0001100 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.7349° |
| argument of perigee: | 98.8136° |
| revolutions per day: | 15.30190356 |
| mean anomaly at epoch: | 261.2990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|