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 40074U 14037F 25341.21839292 .00016693 00000-0 10425-2 0 9990
2 40074 98.4142 320.0176 0003416 82.9918 277.1697 15.09561913619550
| Epoch (UTC): | 07 December 2025 05:14:29 |
| Eccentricity: | 0.0003416 |
| inclination: | 98.4142° |
| perigee height: | 535 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 320.0176° |
| argument of perigee: | 82.9918° |
| revolutions per day: | 15.09561913 |
| mean anomaly at epoch: | 277.1697° |
| orbit number at epoch: | 61955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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