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 40910U 15049M 23080.27798735 .00032542 00000-0 10440-2 0 9991
2 40910 97.4695 92.2997 0013112 83.8225 42.9025 15.32177497415402
| Epoch (UTC): | 21 March 2023 06:40:18 |
| Eccentricity: | 0.0013112 |
| inclination: | 97.4695° |
| perigee height: | 460 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 92.2997° |
| argument of perigee: | 83.8225° |
| revolutions per day: | 15.32177497 |
| mean anomaly at epoch: | 42.9025° |
| orbit number at epoch: | 41540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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