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 13142.16621358 .00000363 00000-0 90584-4 0 1381
2 25994 098.2080 217.4778 0001264 106.1020 254.0365 14.57093635714120
| Epoch (UTC): | 22 May 2013 03:59:20 |
| Eccentricity: | 0.0001264 |
| inclination: | 98.2080° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 217.4778° |
| argument of perigee: | 106.1020° |
| revolutions per day: | 14.57093635 |
| mean anomaly at epoch: | 254.0365° |
| orbit number at epoch: | 71412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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