View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63630U 26145.54336362 +.00000000 +00000-0 +24999-3 0 00007
2 63630 45.4106 93.2616 0004604 84.6415 275.4988 14.98608876 09
| Epoch (UTC): | 25 May 2026 13:02:26 |
| Eccentricity: | 0.0004604 |
| inclination: | 45.4106° |
| perigee height: | 568 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 93.2616° |
| argument of perigee: | 84.6415° |
| revolutions per day: | 14.98608876 |
| mean anomaly at epoch: | 275.4988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|