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 23080.14632761 .00001398 00000-0 23461-3 0 9992
2 00029 48.3786 236.2556 0024260 221.8518 138.0539 14.75129308367105
| Epoch (UTC): | 21 March 2023 03:30:42 |
| Eccentricity: | 0.0024260 |
| inclination: | 48.3786° |
| perigee height: | 628 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 236.2556° |
| argument of perigee: | 221.8518° |
| revolutions per day: | 14.75129308 |
| mean anomaly at epoch: | 138.0539° |
| orbit number at epoch: | 36710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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