View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65830U 26145.54151227 +.00000000 +00000-0 +13951-2 0 00001
2 65830 53.1567 91.8076 0000900 81.2446 278.8657 15.30269746 02
| Epoch (UTC): | 25 May 2026 12:59:46 |
| Eccentricity: | 0.0000900 |
| inclination: | 53.1567° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.8076° |
| argument of perigee: | 81.2446° |
| revolutions per day: | 15.30269746 |
| mean anomaly at epoch: | 278.8657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|