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 42788U 17036Z 19077.11200534 .00001464 00000-0 65851-4 0 9990
2 42788 97.3639 137.1448 0011527 186.9095 173.1985 15.22635642 96263
| Epoch (UTC): | 18 March 2019 02:41:17 |
| Eccentricity: | 0.0011527 |
| inclination: | 97.3639° |
| perigee height: | 490 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 137.1448° |
| argument of perigee: | 186.9095° |
| revolutions per day: | 15.22635642 |
| mean anomaly at epoch: | 173.1985° |
| orbit number at epoch: | 9626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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