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 23083.32032227 .00004307 00000-0 12804-2 0 9993
2 26094 100.1868 207.9705 0033114 323.8785 36.0163 14.43543981214665
| Epoch (UTC): | 24 March 2023 07:41:15 |
| Eccentricity: | 0.0033114 |
| inclination: | 100.1868° |
| perigee height: | 723 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 207.9705° |
| argument of perigee: | 323.8785° |
| revolutions per day: | 14.43543981 |
| mean anomaly at epoch: | 36.0163° |
| orbit number at epoch: | 21466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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