View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25924U 26145.61711272 +.00000000 +00000-0 +00000-0 0 00000
2 25924 0.0139 306.7186 0003950 132.9257 184.7450 1.00276252 08
| Epoch (UTC): | 25 May 2026 14:48:38 |
| Eccentricity: | 0.0003950 |
| inclination: | 0.0139° |
| perigee height: | 35769 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 306.7186° |
| argument of perigee: | 132.9257° |
| revolutions per day: | 1.00276252 |
| mean anomaly at epoch: | 184.7450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|