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 42015U 17008BV 19340.83668644 +.00000868 +00000-0 +37428-4 0 9990
2 42015 097.3836 045.2610 0004763 292.0494 068.0238 15.25195460155835
| Epoch (UTC): | 06 December 2019 20:04:49 |
| Eccentricity: | 0.0004763 |
| inclination: | 97.3836° |
| perigee height: | 487 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 45.2610° |
| argument of perigee: | 292.0494° |
| revolutions per day: | 15.25195460 |
| mean anomaly at epoch: | 68.0238° |
| orbit number at epoch: | 15583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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