View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60092U 26145.12728441 +.00000000 +00000-0 +61256-4 0 00001
2 60092 53.1610 41.7787 0001256 80.2598 279.8545 15.30196864 08
| Epoch (UTC): | 25 May 2026 03:03:17 |
| Eccentricity: | 0.0001256 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 41.7787° |
| argument of perigee: | 80.2598° |
| revolutions per day: | 15.30196864 |
| mean anomaly at epoch: | 279.8545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|