View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47353U 26145.31604105 +.00000000 +00000-0 +97978-4 0 00007
2 47353 53.1602 4.2620 0001681 88.4820 271.6374 15.31707138 07
| Epoch (UTC): | 25 May 2026 07:35:05 |
| Eccentricity: | 0.0001681 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 4.2620° |
| argument of perigee: | 88.4820° |
| revolutions per day: | 15.31707138 |
| mean anomaly at epoch: | 271.6374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|