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 17911U 87038A 24357.52993112 .00019406 00000-0 61137-3 0 9999
2 17911 82.5140 12.8803 0009999 99.9177 260.3194 15.32736017 57182
| Epoch (UTC): | 22 December 2024 12:43:06 |
| Eccentricity: | 0.0009999 |
| inclination: | 82.5140° |
| perigee height: | 461 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 12.8803° |
| argument of perigee: | 99.9177° |
| revolutions per day: | 15.32736017 |
| mean anomaly at epoch: | 260.3194° |
| orbit number at epoch: | 5718 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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