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 116U 61015A 19145.84629663 -.00000028 00000-0 37618-4 0 9995
2 116 66.8106 78.1938 0082749 280.4364 78.7398 13.91753073938225
| Epoch (UTC): | 25 May 2019 20:18:40 |
| Eccentricity: | 0.0082749 |
| inclination: | 66.8106° |
| perigee height: | 862 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 78.1938° |
| argument of perigee: | 280.4364° |
| revolutions per day: | 13.91753073 |
| mean anomaly at epoch: | 78.7398° |
| orbit number at epoch: | 93822 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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