View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64213U 26145.58335647 +.00000000 +00000-0 +14315-2 0 00004
2 64213 53.1611 42.6440 0000956 96.1552 332.1869 15.34359386 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000956 |
| inclination: | 53.1611° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 42.6440° |
| argument of perigee: | 96.1552° |
| revolutions per day: | 15.34359386 |
| mean anomaly at epoch: | 332.1869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|