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 23087U 94023A 22228.67690706 .00000030 00000-0 40523-4 0 9996
2 23087 71.0540 15.8763 0010277 223.5548 136.4764 14.13870787460888
| Epoch (UTC): | 16 August 2022 16:14:44 |
| Eccentricity: | 0.0010277 |
| inclination: | 71.0540° |
| perigee height: | 839 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 15.8763° |
| argument of perigee: | 223.5548° |
| revolutions per day: | 14.13870787 |
| mean anomaly at epoch: | 136.4764° |
| orbit number at epoch: | 46088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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