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 40025U 14033R 23159.62765373 .00004164 00000-0 39728-3 0 9998
2 40025 97.9968 106.2345 0010389 331.0640 29.0002 14.93856512486869
| Epoch (UTC): | 08 June 2023 15:03:49 |
| Eccentricity: | 0.0010389 |
| inclination: | 97.9968° |
| perigee height: | 578 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 106.2345° |
| argument of perigee: | 331.0640° |
| revolutions per day: | 14.93856512 |
| mean anomaly at epoch: | 29.0002° |
| orbit number at epoch: | 48686 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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