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 28894U 05043E 18145.36912715 +.00000044 +00000-0 +17804-4 0 9998
2 28894 097.9270 292.2254 0017679 156.1095 204.0931 14.61522218669844
| Epoch (UTC): | 25 May 2018 08:51:32 |
| Eccentricity: | 0.0017679 |
| inclination: | 97.9270° |
| perigee height: | 676 km |
| apogee height: | 701 km |
| right ascension of ascending node: | 292.2254° |
| argument of perigee: | 156.1095° |
| revolutions per day: | 14.61522218 |
| mean anomaly at epoch: | 204.0931° |
| orbit number at epoch: | 66984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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