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 15027.23938908 .00000316 00000-0 80102-4 0 523
2 25994 098.2024 103.7429 0001428 084.4134 275.7256 14.57116306803695
| Epoch (UTC): | 27 January 2015 05:44:43 |
| Eccentricity: | 0.0001428 |
| inclination: | 98.2024° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 103.7429° |
| argument of perigee: | 84.4134° |
| revolutions per day: | 14.57116306 |
| mean anomaly at epoch: | 275.7256° |
| orbit number at epoch: | 80369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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