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 40907U 15049J 23343.14024709 .00015413 00000-0 44561-3 0 9998
2 40907 97.4874 352.6714 0006747 252.1164 107.9344 15.35702808455263
| Epoch (UTC): | 09 December 2023 03:21:57 |
| Eccentricity: | 0.0006747 |
| inclination: | 97.4874° |
| perigee height: | 454 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 352.6714° |
| argument of perigee: | 252.1164° |
| revolutions per day: | 15.35702808 |
| mean anomaly at epoch: | 107.9344° |
| orbit number at epoch: | 45526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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