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 23087.83350623 .00000381 00000-0 22843-3 0 9993
2 28654 98.9142 162.6014 0013412 245.0048 114.9731 14.12898870920223
| Epoch (UTC): | 28 March 2023 20:00:14 |
| Eccentricity: | 0.0013412 |
| inclination: | 98.9142° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 162.6014° |
| argument of perigee: | 245.0048° |
| revolutions per day: | 14.12898870 |
| mean anomaly at epoch: | 114.9731° |
| orbit number at epoch: | 92022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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