View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65759U 26145.26045630 +.00000000 +00000-0 +94800-3 0 00003
2 65759 53.1610 337.4526 0001156 85.5108 274.6025 15.30211154 09
| Epoch (UTC): | 25 May 2026 06:15:03 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 337.4526° |
| argument of perigee: | 85.5108° |
| revolutions per day: | 15.30211154 |
| mean anomaly at epoch: | 274.6025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|