View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45415U 26145.24221464 +.00000000 +00000-0 +14857-2 0 00002
2 45415 53.1557 131.7917 0006681 27.7140 332.4219 15.37116567 04
| Epoch (UTC): | 25 May 2026 05:48:47 |
| Eccentricity: | 0.0006681 |
| inclination: | 53.1557° |
| perigee height: | 450 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 131.7917° |
| argument of perigee: | 27.7140° |
| revolutions per day: | 15.37116567 |
| mean anomaly at epoch: | 332.4219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|