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 23026.46852594 .00000040 00000-0 90104-4 0 9999
2 116 66.8101 38.3264 0069908 58.0717 302.7136 13.91873041124936
| Epoch (UTC): | 26 January 2023 11:14:40 |
| Eccentricity: | 0.0069908 |
| inclination: | 66.8101° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 38.3264° |
| argument of perigee: | 58.0717° |
| revolutions per day: | 13.91873041 |
| mean anomaly at epoch: | 302.7136° |
| orbit number at epoch: | 12493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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