View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48284U 26145.50730791 +.00000000 +00000-0 +95422-4 0 00005
2 48284 53.1610 78.6065 0001148 96.0987 264.0145 15.31701057 01
| Epoch (UTC): | 25 May 2026 12:10:31 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 78.6065° |
| argument of perigee: | 96.0987° |
| revolutions per day: | 15.31701057 |
| mean anomaly at epoch: | 264.0145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|