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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 25994U 99068A 10040.84431020 .00000032 00000-0 17252-4 0 4955
2 25994 098.2030 117.3116 0001466 066.5124 293.6210 14.57106819539769
| Epoch (UTC): | 8:15:48 PM, Tuesday, February 09, 2010 |
| Eccentricity: | 0.0001466 |
| Inclination: | 098.2030° |
| Perigee Height: | 701 km |
| Apogee Height: | 703 km |
| Right Ascension of Ascending Node: | 117.3116° |
| Argument of Perigee: | 066.5124° |
| Revolutions per Day: | 14.57106819 |
| Mean Anomaly at Epoch: | 293.6210° |
| Orbit Number at Epoch: | 53976 |
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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