View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25994U 99068A 25189.90094197 .00000301 00000-0 70893-4 0 9990
2 25994 97.9969 247.1249 0001494 195.2603 337.8773 14.60728041359607
| Epoch (UTC): | 08 July 2025 21:37:21 |
| Eccentricity: | 0.0001494 |
| inclination: | 97.9969° |
| perigee height: | 690 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 247.1249° |
| argument of perigee: | 195.2603° |
| revolutions per day: | 14.60728041 |
| mean anomaly at epoch: | 337.8773° |
| orbit number at epoch: | 35960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|