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 24680U 96072A 13135.85157678 0.00013000 00000-0 22429-3 0 03
2 24680 97.5795 189.5830 0339063 344.4401 15.5597 15.06427399 00
| Epoch (UTC): | 15 May 2013 20:26:16 |
| Eccentricity: | 0.0339063 |
| inclination: | 97.5795° |
| perigee height: | 312 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 189.5830° |
| argument of perigee: | 344.4401° |
| revolutions per day: | 15.06427399 |
| mean anomaly at epoch: | 15.5597° |
| 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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