View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64813U 26145.14410280 +.00000000 +00000-0 +16683-3 0 00000
2 64813 70.0003 301.8919 0002810 269.4720 90.6117 14.98334980 09
| Epoch (UTC): | 25 May 2026 03:27:30 |
| Eccentricity: | 0.0002810 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.8919° |
| argument of perigee: | 269.4720° |
| revolutions per day: | 14.98334980 |
| mean anomaly at epoch: | 90.6117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|