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 116U 61015A 23030.27687266 .00000026 00000-0 79008-4 0 9999
2 116 66.8104 29.0145 0070103 55.1655 305.5991 13.91873825125461
| Epoch (UTC): | 30 January 2023 06:38:41 |
| Eccentricity: | 0.0070103 |
| inclination: | 66.8104° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 29.0145° |
| argument of perigee: | 55.1655° |
| revolutions per day: | 13.91873825 |
| mean anomaly at epoch: | 305.5991° |
| orbit number at epoch: | 12546 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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