View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41394U 26145.62395428 +.00000000 +00000-0 +10405-3 0 00004
2 41394 97.9774 160.2508 0024251 22.8537 337.3764 15.07868422 05
| Epoch (UTC): | 25 May 2026 14:58:29 |
| Eccentricity: | 0.0024251 |
| inclination: | 97.9774° |
| perigee height: | 526 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 160.2508° |
| argument of perigee: | 22.8537° |
| revolutions per day: | 15.07868422 |
| mean anomaly at epoch: | 337.3764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|