View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63034U 26145.58485985 +.00000000 +00000-0 +10281-2 0 00003
2 63034 53.1586 260.6838 0001565 94.7889 265.3292 15.31745260 04
| Epoch (UTC): | 25 May 2026 14:02:11 |
| Eccentricity: | 0.0001565 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 260.6838° |
| argument of perigee: | 94.7889° |
| revolutions per day: | 15.31745260 |
| mean anomaly at epoch: | 265.3292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|