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 23156.14357046 .00026415 00000-0 72731-3 0 9991
2 40910 97.4612 169.0995 0011008 155.9059 204.2703 15.37074941427033
| Epoch (UTC): | 05 June 2023 03:26:44 |
| Eccentricity: | 0.0011008 |
| inclination: | 97.4612° |
| perigee height: | 447 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 169.0995° |
| argument of perigee: | 155.9059° |
| revolutions per day: | 15.37074941 |
| mean anomaly at epoch: | 204.2703° |
| orbit number at epoch: | 42703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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