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 28888U 05042A 13169.83465417 0.00023000 00000-0 22700-3 0 05
2 28888 97.9433 232.7817 0545725 80.6590 279.3409 14.74638366 09
| Epoch (UTC): | 18 June 2013 20:01:54 |
| Eccentricity: | 0.0545725 |
| inclination: | 97.9433° |
| perigee height: | 263 km |
| apogee height: | 1029 km |
| right ascension of ascending node: | 232.7817° |
| argument of perigee: | 80.6590° |
| revolutions per day: | 14.74638366 |
| mean anomaly at epoch: | 279.3409° |
| 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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