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 26929U 01043A 03021.14417834 .23075867 62110-5 22771-3 0 9999
2 26929 067.0082 058.0340 0002739 336.9161 023.5083 16.51128562 74338
Epoch (UTC): | 21 January 2003 03:27:37 |
Eccentricity: | 0.0002739 |
inclination: | 67.0082° |
perigee height: | 134 km |
apogee height: | 138 km |
right ascension of ascending node: | 58.0340° |
argument of perigee: | 336.9161° |
revolutions per day: | 16.51128562 |
mean anomaly at epoch: | 23.5083° |
orbit number at epoch: | 7433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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