View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66234U 26145.11093587 +.00000000 +00000-0 +13070-2 0 00009
2 66234 53.1582 288.4568 0000667 109.8522 250.2551 15.31758664 00
| Epoch (UTC): | 25 May 2026 02:39:44 |
| Eccentricity: | 0.0000667 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 288.4568° |
| argument of perigee: | 109.8522° |
| revolutions per day: | 15.31758664 |
| mean anomaly at epoch: | 250.2551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|