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 28375U 04025K 13144.91610088 .00000299 00000-0 10150-3 0 5651
2 28375 098.1994 101.3116 0084816 086.8046 306.9444 14.41115378467988
| Epoch (UTC): | 24 May 2013 21:59:11 |
| Eccentricity: | 0.0084816 |
| inclination: | 98.1994° |
| perigee height: | 694 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 101.3116° |
| argument of perigee: | 86.8046° |
| revolutions per day: | 14.41115378 |
| mean anomaly at epoch: | 306.9444° |
| orbit number at epoch: | 46798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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