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 40095U 14041A 14244.13927022 .00091428 86473-5 38448-3 0 9996
2 40095 064.8767 133.1687 0204309 045.9666 107.3536 15.60523747 6888
| Epoch (UTC): | 01 September 2014 03:20:32 |
| Eccentricity: | 0.0204309 |
| inclination: | 64.8767° |
| perigee height: | 248 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 133.1687° |
| argument of perigee: | 45.9666° |
| revolutions per day: | 15.60523747 |
| mean anomaly at epoch: | 107.3536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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