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 28654U 05018A 22178.90055056 .00000136 00000-0 97630-4 0 9998
2 28654 98.9488 249.3283 0013229 304.2715 55.7203 14.12746593881453
| Epoch (UTC): | 27 June 2022 21:36:47 |
| Eccentricity: | 0.0013229 |
| inclination: | 98.9488° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 249.3283° |
| argument of perigee: | 304.2715° |
| revolutions per day: | 14.12746593 |
| mean anomaly at epoch: | 55.7203° |
| orbit number at epoch: | 88145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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