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 00116U 61015A 23263.87251096 .00000099 00000-0 13392-3 0 9994
2 00116 66.8102 177.8211 0082321 255.5737 103.6196 13.91944989157466
| Epoch (UTC): | 20 September 2023 20:56:24 |
| Eccentricity: | 0.0082321 |
| inclination: | 66.8102° |
| perigee height: | 862 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 177.8211° |
| argument of perigee: | 255.5737° |
| revolutions per day: | 13.91944989 |
| mean anomaly at epoch: | 103.6196° |
| orbit number at epoch: | 15746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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