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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 09319.79534688 0.00004300 00000-0 68166-4 0 07
2 24680 97.8170 10.2441 0454915 303.4297 56.5702 14.84853973 09
| Epoch (UTC): | 7:05:18 PM, Sunday, November 15, 2009 |
| Eccentricity: | 0.0454915 |
| Inclination: | 97.8170° |
| Perigee Height: | 296 km |
| Apogee Height: | 932 km |
| Right Ascension of Ascending Node: | 10.2441° |
| Argument of Perigee: | 303.4297° |
| Revolutions per Day: | 14.84853973 |
| Mean Anomaly at Epoch: | 56.5702° |
| 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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