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 29252U 06029A 13169.59775818 .00002204 00000-0 14273-3 0 9232
2 29252 064.5110 346.7297 0009169 203.0142 157.1077 15.07880466380974
| Epoch (UTC): | 18 June 2013 14:20:46 |
| Eccentricity: | 0.0009169 |
| inclination: | 64.5110° |
| perigee height: | 536 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 346.7297° |
| argument of perigee: | 203.0142° |
| revolutions per day: | 15.07880466 |
| mean anomaly at epoch: | 157.1077° |
| orbit number at epoch: | 38097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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