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 25289U 98021E 13169.43159220 .00000234 00000-0 76383-4 0 2670
2 25289 086.3985 113.9809 0002409 101.3148 048.5215 14.34219347795780
| Epoch (UTC): | 18 June 2013 10:21:29 |
| Eccentricity: | 0.0002409 |
| inclination: | 86.3985° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 113.9809° |
| argument of perigee: | 101.3148° |
| revolutions per day: | 14.34219347 |
| mean anomaly at epoch: | 48.5215° |
| orbit number at epoch: | 79578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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