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 23080.83355861 .00007160 00000-0 69617-3 0 9990
2 40025 97.9892 26.1424 0010137 216.5132 143.5396 14.92848044475100
| Epoch (UTC): | 21 March 2023 20:00:19 |
| Eccentricity: | 0.0010137 |
| inclination: | 97.9892° |
| perigee height: | 582 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 26.1424° |
| argument of perigee: | 216.5132° |
| revolutions per day: | 14.92848044 |
| mean anomaly at epoch: | 143.5396° |
| orbit number at epoch: | 47510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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