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 is defined by the following mean orbital elements,
1 35002U 09028B 12226.86484473 .07728342 73476-5 57159-3 0 9991
2 35002 040.4341 050.6671 0012079 300.9773 059.0492 16.39309245183554
| Epoch (UTC): | 13 August 2012 20:45:22 |
| Eccentricity: | 0.0012079 |
| inclination: | 40.4341° |
| perigee height: | 160 km |
| apogee height: | 175 km |
| right ascension of ascending node: | 50.6671° |
| argument of perigee: | 300.9773° |
| revolutions per day: | 16.39309245 |
| mean anomaly at epoch: | 59.0492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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