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 59U 60013B 19176.46922035 +.00000096 +00000-0 +82419-5 0 9993
2 59 028.2479 257.0795 0189106 161.5046 199.2484 13.52968485898082
| Epoch (UTC): | 25 June 2019 11:15:40 |
| Eccentricity: | 0.0189106 |
| inclination: | 28.2479° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 257.0795° |
| argument of perigee: | 161.5046° |
| revolutions per day: | 13.52968485 |
| mean anomaly at epoch: | 199.2484° |
| orbit number at epoch: | 89808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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