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 40887U 15044A 23081.45813383 -.00000107 00000-0 00000+0 0 9998
2 40887 2.6498 18.4075 0058542 358.4471 42.7960 1.00271540 27691
| Epoch (UTC): | 22 March 2023 10:59:42 |
| Eccentricity: | 0.0058542 |
| inclination: | 2.6498° |
| perigee height: | 35539 km |
| apogee height: | 36033 km |
| right ascension of ascending node: | 18.4075° |
| argument of perigee: | 358.4471° |
| revolutions per day: | 1.00271540 |
| mean anomaly at epoch: | 42.7960° |
| orbit number at epoch: | 2769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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