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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 28376U 04026A 09323.19282144 .00000028 00000-0 16154-4 0 6534
2 28376 098.1938 264.9449 0001171 070.5423 289.5899 14.57114452284384
| Epoch (UTC): | 4:37:40 AM, Thursday, November 19, 2009 |
| Eccentricity: | 0.0001171 |
| Inclination: | 098.1938° |
| Perigee Height: | 701 km |
| Apogee Height: | 703 km |
| Right Ascension of Ascending Node: | 264.9449° |
| Argument of Perigee: | 070.5423° |
| Revolutions per Day: | 14.57114452 |
| Mean Anomaly at Epoch: | 289.5899° |
| Orbit Number at Epoch: | 28438 |
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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