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 23337.42920985 .00001892 00000-0 56443-3 0 9997
2 26094 100.2164 152.2536 0032981 319.0147 40.8560 14.44247045251308
| Epoch (UTC): | 03 December 2023 10:18:03 |
| Eccentricity: | 0.0032981 |
| inclination: | 100.2164° |
| perigee height: | 721 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 152.2536° |
| argument of perigee: | 319.0147° |
| revolutions per day: | 14.44247045 |
| mean anomaly at epoch: | 40.8560° |
| orbit number at epoch: | 25130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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