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 28895U 05043F 19083.16580882 .00000093 00000-0 26751-4 0 9990
2 28895 97.9443 228.9324 0015444 264.0017 95.9426 14.63640625714822
| Epoch (UTC): | 24 March 2019 03:58:45 |
| Eccentricity: | 0.0015444 |
| inclination: | 97.9443° |
| perigee height: | 670 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 228.9324° |
| argument of perigee: | 264.0017° |
| revolutions per day: | 14.63640625 |
| mean anomaly at epoch: | 95.9426° |
| orbit number at epoch: | 71482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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