View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64621U 26145.43401051 +.00000000 +00000-0 +18126-3 0 00009
2 64621 97.4347 148.2706 0012877 216.1730 143.8635 15.18003546 01
| Epoch (UTC): | 25 May 2026 10:24:58 |
| Eccentricity: | 0.0012877 |
| inclination: | 97.4347° |
| perigee height: | 503 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 148.2706° |
| argument of perigee: | 216.1730° |
| revolutions per day: | 15.18003546 |
| mean anomaly at epoch: | 143.8635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|