View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47887U 26145.66482791 +.00000000 +00000-0 +19892-3 0 00000
2 47887 53.1583 282.9641 0001174 83.2268 276.8867 15.31712986 02
| Epoch (UTC): | 25 May 2026 15:57:21 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 282.9641° |
| argument of perigee: | 83.2268° |
| revolutions per day: | 15.31712986 |
| mean anomaly at epoch: | 276.8867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|