View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57815U 26145.43765655 +.00000000 +00000-0 +24034-4 0 00005
2 57815 43.0034 160.9496 0001667 289.7458 70.3214 15.27579076 06
| Epoch (UTC): | 25 May 2026 10:30:13 |
| Eccentricity: | 0.0001667 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.9496° |
| argument of perigee: | 289.7458° |
| revolutions per day: | 15.27579076 |
| mean anomaly at epoch: | 70.3214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|