View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48274U 26041.38023602 +.00000000 +00000-0 +28372-3 0 00000
2 48274 41.4682 14.1762 0004477 48.6892 311.4331 15.59430362 06
| Epoch (UTC): | 10 February 2026 09:07:32 |
| Eccentricity: | 0.0004477 |
| inclination: | 41.4682° |
| perigee height: | 386 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 14.1762° |
| argument of perigee: | 48.6892° |
| revolutions per day: | 15.59430362 |
| mean anomaly at epoch: | 311.4331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|