View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62759U 26145.51702508 +.00000000 +00000-0 +75845-3 0 00000
2 62759 53.1593 325.6112 0000657 10.9747 349.1269 15.31721784 06
| Epoch (UTC): | 25 May 2026 12:24:30 |
| Eccentricity: | 0.0000657 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 325.6112° |
| argument of perigee: | 10.9747° |
| revolutions per day: | 15.31721784 |
| mean anomaly at epoch: | 349.1269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|