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 40057U 14034E 23155.57514425 .00003127 00000-0 40283-3 0 9990
2 40057 98.3717 348.0445 0008722 284.6510 75.3734 14.81828105481567
| Epoch (UTC): | 04 June 2023 13:48:12 |
| Eccentricity: | 0.0008722 |
| inclination: | 98.3717° |
| perigee height: | 617 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 348.0445° |
| argument of perigee: | 284.6510° |
| revolutions per day: | 14.81828105 |
| mean anomaly at epoch: | 75.3734° |
| orbit number at epoch: | 48156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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