View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63029U 26144.87677301 +.00000000 +00000-0 +39079-3 0 00000
2 63029 53.1588 276.8711 0001119 89.2281 270.8848 15.30208025 09
| Epoch (UTC): | 24 May 2026 21:02:33 |
| Eccentricity: | 0.0001119 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 276.8711° |
| argument of perigee: | 89.2281° |
| revolutions per day: | 15.30208025 |
| mean anomaly at epoch: | 270.8848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|