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 40900U 15049B 22135.81207745 .00027096 00000-0 81893-3 0 9995
2 40900 97.4027 153.6515 0011007 59.0924 115.1374 15.34143443369606
| Epoch (UTC): | 15 May 2022 19:29:23 |
| Eccentricity: | 0.0011007 |
| inclination: | 97.4027° |
| perigee height: | 456 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 153.6515° |
| argument of perigee: | 59.0924° |
| revolutions per day: | 15.34143443 |
| mean anomaly at epoch: | 115.1374° |
| orbit number at epoch: | 36960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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