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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 26626U 00077A 09322.06455736 -.00000170 +00000-0 +10000-3 0 05076
2 26626 064.1768 013.9814 2655524 270.7007 059.3581 01.00279148032855
| Epoch (UTC): | 1:32:58 AM, Wednesday, November 18, 2009 |
| Eccentricity: | 0.2655524 |
| Inclination: | 064.1768° |
| Perigee Height: | 24,588 km |
| Apogee Height: | 46,980 km |
| Right Ascension of Ascending Node: | 013.9814° |
| Argument of Perigee: | 270.7007° |
| Revolutions per Day: | 01.00279148 |
| Mean Anomaly at Epoch: | 059.3581° |
| Orbit Number at Epoch: | 03285 |
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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