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 40024U 14033Q 25342.98414825 .00020455 00000-0 83512-3 0 9996
2 40024 98.0901 354.3436 0005533 113.2346 246.9473 15.24430060624937
| Epoch (UTC): | 08 December 2025 23:37:10 |
| Eccentricity: | 0.0005533 |
| inclination: | 98.0901° |
| perigee height: | 489 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 354.3436° |
| argument of perigee: | 113.2346° |
| revolutions per day: | 15.24430060 |
| mean anomaly at epoch: | 246.9473° |
| orbit number at epoch: | 62493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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