View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66739U 26145.16106594 +.00000000 +00000-0 +25429-3 0 00009
2 66739 97.4248 219.3389 0003680 62.5940 297.5669 15.20115741 06
| Epoch (UTC): | 25 May 2026 03:51:56 |
| Eccentricity: | 0.0003680 |
| inclination: | 97.4248° |
| perigee height: | 503 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 219.3389° |
| argument of perigee: | 62.5940° |
| revolutions per day: | 15.20115741 |
| mean anomaly at epoch: | 297.5669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|