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 23774U 96004B 25199.82112147 .00000102 00000-0 87590-4 0 9990
2 23774 82.9811 338.6553 0043702 2.3690 357.7666 13.76817064481919
| Epoch (UTC): | 18 July 2025 19:42:24 |
| Eccentricity: | 0.0043702 |
| inclination: | 82.9811° |
| perigee height: | 943 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 338.6553° |
| argument of perigee: | 2.3690° |
| revolutions per day: | 13.76817064 |
| mean anomaly at epoch: | 357.7666° |
| orbit number at epoch: | 48191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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