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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 10040.45866121 .00000018 00000-0 13987-4 0 7209
2 28376 098.2038 345.9330 0001395 094.7667 265.3680 14.57109368296362
| Epoch (UTC): | 11:00:28 AM, Tuesday, February 09, 2010 |
| Eccentricity: | 0.0001395 |
| Inclination: | 098.2038° |
| Perigee Height: | 701 km |
| Apogee Height: | 703 km |
| Right Ascension of Ascending Node: | 345.9330° |
| Argument of Perigee: | 094.7667° |
| Revolutions per Day: | 14.57109368 |
| Mean Anomaly at Epoch: | 265.3680° |
| Orbit Number at Epoch: | 29636 |
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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