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 10489U 77108A 23081.28660240 .00000083 00000-0 00000+0 0 9997
2 10489 8.0321 294.9771 0011597 74.7115 289.8975 1.00307799125399
| Epoch (UTC): | 22 March 2023 06:52:42 |
| Eccentricity: | 0.0011597 |
| inclination: | 8.0321° |
| perigee height: | 35727 km |
| apogee height: | 35825 km |
| right ascension of ascending node: | 294.9771° |
| argument of perigee: | 74.7115° |
| revolutions per day: | 1.00307799 |
| mean anomaly at epoch: | 289.8975° |
| orbit number at epoch: | 12539 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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