View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57853U 26145.11017726 +.00000000 +00000-0 +14395-4 0 00000
2 57853 53.1609 288.7789 0001102 98.1432 261.9694 15.30189653 02
| Epoch (UTC): | 25 May 2026 02:38:39 |
| Eccentricity: | 0.0001102 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.7789° |
| argument of perigee: | 98.1432° |
| revolutions per day: | 15.30189653 |
| mean anomaly at epoch: | 261.9694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|