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 28538U 05004B 13135.89071039 0.00000050 00000-0 76308-4 0 01
2 28538 63.8210 102.3978 0215000 273.0235 86.9765 13.42986161 00
| Epoch (UTC): | 15 May 2013 21:22:37 |
| Eccentricity: | 0.0215000 |
| inclination: | 63.8210° |
| perigee height: | 937 km |
| apogee height: | 1259 km |
| right ascension of ascending node: | 102.3978° |
| argument of perigee: | 273.0235° |
| revolutions per day: | 13.42986161 |
| mean anomaly at epoch: | 86.9765° |
| 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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