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 23081.83896287 .00007539 00000-0 73240-3 0 9990
2 40025 97.9894 27.1630 0010224 212.6097 147.4491 14.92864015475763
| Epoch (UTC): | 22 March 2023 20:08:06 |
| Eccentricity: | 0.0010224 |
| inclination: | 97.9894° |
| perigee height: | 582 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 27.1630° |
| argument of perigee: | 212.6097° |
| revolutions per day: | 14.92864015 |
| mean anomaly at epoch: | 147.4491° |
| orbit number at epoch: | 47576 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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