View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64462U 26145.13352903 +.00000000 +00000-0 +62625-3 0 00003
2 64462 53.1595 95.7594 0001251 78.4131 281.7011 15.31718895 02
| Epoch (UTC): | 25 May 2026 03:12:16 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.7594° |
| argument of perigee: | 78.4131° |
| revolutions per day: | 15.31718895 |
| mean anomaly at epoch: | 281.7011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|