View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57176U 26145.55967405 +.00000000 +00000-0 +40763-3 0 00001
2 57176 97.5074 209.2526 0011920 174.7749 185.3617 15.28846171 02
| Epoch (UTC): | 25 May 2026 13:25:55 |
| Eccentricity: | 0.0011920 |
| inclination: | 97.5074° |
| perigee height: | 471 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 209.2526° |
| argument of perigee: | 174.7749° |
| revolutions per day: | 15.28846171 |
| mean anomaly at epoch: | 185.3617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|