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 28095U 03054A 21062.09035344 0.00000000 00000-0 00000-0 0 08
2 28095 63.4194 89.3025 0429331 359.5500 0.4846 13.41400721 04
| Epoch (UTC): | 03 March 2021 02:10:06 |
| Eccentricity: | 0.0429331 |
| inclination: | 63.4194° |
| perigee height: | 783 km |
| apogee height: | 1425 km |
| right ascension of ascending node: | 89.3025° |
| argument of perigee: | 359.5500° |
| revolutions per day: | 13.41400721 |
| mean anomaly at epoch: | 0.4846° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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