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 61873U 24203E 24358.23997475 .00013832 00000-0 59580-3 0 9991
2 61873 97.3801 61.8087 0099360 349.8358 10.0864 15.18246809 6685
| Epoch (UTC): | 23 December 2024 05:45:33 |
| Eccentricity: | 0.0099360 |
| inclination: | 97.3801° |
| perigee height: | 442 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 61.8087° |
| argument of perigee: | 349.8358° |
| revolutions per day: | 15.18246809 |
| mean anomaly at epoch: | 10.0864° |
| orbit number at epoch: | 668 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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