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 40071U 14037C 22175.76422548 .00000736 00000-0 10044-3 0 9990
2 40071 98.4083 44.8663 0007257 298.9365 61.1115 14.81880789430422
| Epoch (UTC): | 24 June 2022 18:20:29 |
| Eccentricity: | 0.0007257 |
| inclination: | 98.4083° |
| perigee height: | 618 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 44.8663° |
| argument of perigee: | 298.9365° |
| revolutions per day: | 14.81880789 |
| mean anomaly at epoch: | 61.1115° |
| orbit number at epoch: | 43042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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