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 40071U 14037C 25013.12426349 .00002777 00000-0 31653-3 0 9993
2 40071 98.3374 301.4349 0008020 152.8411 207.3225 14.87016775568819
| Epoch (UTC): | 13 January 2025 02:58:56 |
| Eccentricity: | 0.0008020 |
| inclination: | 98.3374° |
| perigee height: | 601 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 301.4349° |
| argument of perigee: | 152.8411° |
| revolutions per day: | 14.87016775 |
| mean anomaly at epoch: | 207.3225° |
| orbit number at epoch: | 56881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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