View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 43784U 18099AC 25349.93515777 .00008622 00000-0 37656-3 0 9998
2 43784 97.4171 41.3455 0002560 186.2520 173.8685 15.22354318385396
| Epoch (UTC): | 15 December 2025 22:26:37 |
| Eccentricity: | 0.0002560 |
| inclination: | 97.4171° |
| perigee height: | 497 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 41.3455° |
| argument of perigee: | 186.2520° |
| revolutions per day: | 15.22354318 |
| mean anomaly at epoch: | 173.8685° |
| orbit number at epoch: | 38539 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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