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 40014U 14033E 23159.81708962 .00003611 00000-0 29732-3 0 9998
2 40014 98.1406 178.4107 0028102 301.5768 58.2711 14.99484715489467
| Epoch (UTC): | 08 June 2023 19:36:36 |
| Eccentricity: | 0.0028102 |
| inclination: | 98.1406° |
| perigee height: | 549 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 178.4107° |
| argument of perigee: | 301.5768° |
| revolutions per day: | 14.99484715 |
| mean anomaly at epoch: | 58.2711° |
| orbit number at epoch: | 48946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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