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 40015U 14033F 22176.86012219 .00000378 00000-0 57368-4 0 9999
2 40015 97.6410 30.4239 0038290 76.0088 284.5377 14.78921639432578
| Epoch (UTC): | 25 June 2022 20:38:34 |
| Eccentricity: | 0.0038290 |
| inclination: | 97.6410° |
| perigee height: | 606 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 30.4239° |
| argument of perigee: | 76.0088° |
| revolutions per day: | 14.78921639 |
| mean anomaly at epoch: | 284.5377° |
| orbit number at epoch: | 43257 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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