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 39227U 13042A 24358.12048522 .00004457 00000-0 32231-3 0 9993
2 39227 97.6166 181.3827 0003070 148.6500 211.4909 15.04533237622564
| Epoch (UTC): | 23 December 2024 02:53:29 |
| Eccentricity: | 0.0003070 |
| inclination: | 97.6166° |
| perigee height: | 551 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 181.3827° |
| argument of perigee: | 148.6500° |
| revolutions per day: | 15.04533237 |
| mean anomaly at epoch: | 211.4909° |
| orbit number at epoch: | 62256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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