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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 25744U 99028A 05334.15210437 0.00000000 00000-0 00000-0 0 01
2 25744 63.4412 124.9814 0242000 294.1240 65.8760 9.69817792 03
| Epoch (UTC): | 3:39:02 AM, Wednesday, November 30, 2005 |
| Eccentricity: | 0.0242000 |
| Inclination: | 63.4412° |
| Perigee Height: | 2,685 km |
| Apogee Height: | 3,135 km |
| Right Ascension of Ascending Node: | 124.9814° |
| Argument of Perigee: | 294.1240° |
| Revolutions per Day: | 9.69817792 |
| Mean Anomaly at Epoch: | 65.8760° |
| 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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