View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62630U 26145.44214332 +.00000000 +00000-0 +67821-4 0 00009
2 62630 97.4857 219.2904 0004049 199.3234 160.7840 15.05144357 05
| Epoch (UTC): | 25 May 2026 10:36:41 |
| Eccentricity: | 0.0004049 |
| inclination: | 97.4857° |
| perigee height: | 548 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 219.2904° |
| argument of perigee: | 199.3234° |
| revolutions per day: | 15.05144357 |
| mean anomaly at epoch: | 160.7840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|