View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17528U 26041.94253338 +.00000000 +00000-0 +14857-3 0 00004
2 17528 97.4026 50.5403 0145911 97.4804 264.3000 14.54431733 03
| Epoch (UTC): | 10 February 2026 22:37:14 |
| Eccentricity: | 0.0145911 |
| inclination: | 97.4026° |
| perigee height: | 608 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 50.5403° |
| argument of perigee: | 97.4804° |
| revolutions per day: | 14.54431733 |
| mean anomaly at epoch: | 264.3000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|