View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62104U 26145.34903723 +.00000000 +00000-0 +62400-3 0 00000
2 62104 43.0054 132.7493 0001444 262.6986 97.3702 15.27586521 02
| Epoch (UTC): | 25 May 2026 08:22:36 |
| Eccentricity: | 0.0001444 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.7493° |
| argument of perigee: | 262.6986° |
| revolutions per day: | 15.27586521 |
| mean anomaly at epoch: | 97.3702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|