2. Tilt view +68° high towards SE (135°) for peak brightness.
3. Follow the satellite as it sets on the horizon towards NE (045°).
| SATELLITE | NORAD | MAG (BRIGHTNESS) | AOS (RISE) | TCA (PEAK ELEVATION) | LOS (SET) | SKY TRAJECTORY | ILLUMINATION | ACTION |
|---|
| SATELLITE | NORAD | MAG (BRIGHTNESS) | AOS (RISE) | TCA (PEAK ELEVATION) | LOS (SET) | SKY TRAJECTORY | ILLUMINATION | ACTION |
|---|
OrbitAlert calculates observer-specific topocentric satellite passes over 48-hour forward windows for any global latitude and longitude. Telemetry includes Acquisition of Signal (AOS), Time of Closest Approach (TCA), Loss of Signal (LOS), azimuth compass bearings, and maximum elevation angles.
True optical visibility requires two independent astronomical conditions: the ground observer must be in darkness (sun elevation < -6° civil twilight) AND the spacecraft must be directly illuminated by sunlight outside the cylindrical Earth shadow (umbra). Satellites in eclipse are flagged as invisible to the naked eye.
Ingests real-time solar wind velocities, planetary Kp indices, and geomagnetic storm scales (G0 Nominal through G5 Extreme) from the NOAA Space Weather Prediction Center (SWPC). Conjunction proximity screening and decaying orbit re-entry notifications are provided for educational and situational awareness purposes.