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 23160.88477577 .00003301 00000-0 27222-3 0 9990
2 40014 98.1406 179.5265 0028137 297.7726 62.0644 14.99491523489623
| Epoch (UTC): | 09 June 2023 21:14:04 |
| Eccentricity: | 0.0028137 |
| inclination: | 98.1406° |
| perigee height: | 549 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 179.5265° |
| argument of perigee: | 297.7726° |
| revolutions per day: | 14.99491523 |
| mean anomaly at epoch: | 62.0644° |
| orbit number at epoch: | 48962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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