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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 10036.44411713 0.00005100 00000-0 78632-4 0 08
2 24680 97.7880 90.4220 0453415 34.5985 325.4014 14.85736937 06
| Epoch (UTC): | 10:39:32 AM, Friday, February 05, 2010 |
| Eccentricity: | 0.0453415 |
| Inclination: | 97.7880° |
| Perigee Height: | 294 km |
| Apogee Height: | 928 km |
| Right Ascension of Ascending Node: | 90.4220° |
| Argument of Perigee: | 34.5985° |
| Revolutions per Day: | 14.85736937 |
| Mean Anomaly at Epoch: | 325.4014° |
| Orbit Number at Epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
and the full part is where it is sunlit.
Developed and maintained by
Chris Peat, Heavens-Above GmbH
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