View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24725U 26088.20541016 +.00000000 +00000-0 +73721-4 0 00000
2 24725 82.6119 330.8621 0008459 309.4590 50.5751 12.60723008 00
| Epoch (UTC): | 29 March 2026 04:55:47 |
| Eccentricity: | 0.0008459 |
| inclination: | 82.6119° |
| perigee height: | 1413 km |
| apogee height: | 1427 km |
| right ascension of ascending node: | 330.8621° |
| argument of perigee: | 309.4590° |
| revolutions per day: | 12.60723008 |
| mean anomaly at epoch: | 50.5751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|