View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60464U 26145.62227492 +.00000000 +00000-0 +22353-3 0 00003
2 60464 35.0042 292.1935 0007018 297.4684 62.5319 15.29489315 06
| Epoch (UTC): | 25 May 2026 14:56:04 |
| Eccentricity: | 0.0007018 |
| inclination: | 35.0042° |
| perigee height: | 473 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 292.1935° |
| argument of perigee: | 297.4684° |
| revolutions per day: | 15.29489315 |
| mean anomaly at epoch: | 62.5319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|