View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63357U 26145.39328479 +.00000000 +00000-0 +20447-3 0 00000
2 63357 97.5597 121.4311 0017856 333.0219 27.0083 15.14393528 00
| Epoch (UTC): | 25 May 2026 09:26:19 |
| Eccentricity: | 0.0017856 |
| inclination: | 97.5597° |
| perigee height: | 510 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 121.4311° |
| argument of perigee: | 333.0219° |
| revolutions per day: | 15.14393528 |
| mean anomaly at epoch: | 27.0083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|