View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68025U 26145.36469027 +.00000000 +00000-0 +66829-3 0 00003
2 68025 97.2858 94.3756 0002007 113.3362 246.8092 15.33446396 09
| Epoch (UTC): | 25 May 2026 08:45:09 |
| Eccentricity: | 0.0002007 |
| inclination: | 97.2858° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3756° |
| argument of perigee: | 113.3362° |
| revolutions per day: | 15.33446396 |
| mean anomaly at epoch: | 246.8092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|