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 26094U 00004M 23273.41155014 .00001734 00000-0 52087-3 0 9993
2 26094 100.2158 75.4727 0033855 140.4620 219.9043 14.44020706242096
| Epoch (UTC): | 30 September 2023 09:52:37 |
| Eccentricity: | 0.0033855 |
| inclination: | 100.2158° |
| perigee height: | 721 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 75.4727° |
| argument of perigee: | 140.4620° |
| revolutions per day: | 14.44020706 |
| mean anomaly at epoch: | 219.9043° |
| orbit number at epoch: | 24209 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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