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 42000U 17008BE 18140.60497504 +.00000941 +00000-0 +42813-4 0 9997
2 42000 097.4498 205.2166 0010364 106.6210 253.6165 15.23141402069209
| Epoch (UTC): | 20 May 2018 14:31:09 |
| Eccentricity: | 0.0010364 |
| inclination: | 97.4498° |
| perigee height: | 489 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 205.2166° |
| argument of perigee: | 106.6210° |
| revolutions per day: | 15.23141402 |
| mean anomaly at epoch: | 253.6165° |
| orbit number at epoch: | 6920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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