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 00029U 60002B 23038.21557493 .00000943 00000-0 16884-3 0 9997
2 00029 48.3797 74.3579 0023515 39.8763 320.3871 14.74976119360910
| Epoch (UTC): | 07 February 2023 05:10:25 |
| Eccentricity: | 0.0023515 |
| inclination: | 48.3797° |
| perigee height: | 629 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 74.3579° |
| argument of perigee: | 39.8763° |
| revolutions per day: | 14.74976119 |
| mean anomaly at epoch: | 320.3871° |
| orbit number at epoch: | 36091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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