View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44703U 26145.64082108 +.00000000 +00000-0 +17184-3 0 00002
2 44703 97.2441 207.9526 0018186 113.2334 247.0820 15.21396459 07
| Epoch (UTC): | 25 May 2026 15:22:46 |
| Eccentricity: | 0.0018186 |
| inclination: | 97.2441° |
| perigee height: | 489 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 207.9526° |
| argument of perigee: | 113.2334° |
| revolutions per day: | 15.21396459 |
| mean anomaly at epoch: | 247.0820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|