View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64214U 26144.98850632 +.00000000 +00000-0 +90846-3 0 00008
2 64214 53.1602 44.0542 0001095 82.5481 277.5646 15.34410037 03
| Epoch (UTC): | 24 May 2026 23:43:26 |
| Eccentricity: | 0.0001095 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 44.0542° |
| argument of perigee: | 82.5481° |
| revolutions per day: | 15.34410037 |
| mean anomaly at epoch: | 277.5646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|