View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64533U 26145.57906367 +.00000000 +00000-0 +14682-3 0 00009
2 64533 97.4660 260.7017 0003636 266.5752 93.5067 15.21241138 07
| Epoch (UTC): | 25 May 2026 13:53:51 |
| Eccentricity: | 0.0003636 |
| inclination: | 97.4660° |
| perigee height: | 500 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 260.7017° |
| argument of perigee: | 266.5752° |
| revolutions per day: | 15.21241138 |
| mean anomaly at epoch: | 93.5067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|