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 23851U 96024A 13133.08351709 0.00000030 00000-0 21175-4 0 00
2 23851 98.8196 190.8006 0010000 146.9182 213.0817 13.97934665 03
| Epoch (UTC): | 13 May 2013 02:00:15 |
| Eccentricity: | 0.0010000 |
| inclination: | 98.8196° |
| perigee height: | 893 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 190.8006° |
| argument of perigee: | 146.9182° |
| revolutions per day: | 13.97934665 |
| mean anomaly at epoch: | 213.0817° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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