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 01002U 65008C 23265.30611494 .00000025 00000-0 21683-2 0 9997
2 01002 32.1408 251.0150 0014265 260.6806 99.2078 9.88353975117363
| Epoch (UTC): | 22 September 2023 07:20:48 |
| Eccentricity: | 0.0014265 |
| inclination: | 32.1408° |
| perigee height: | 2780 km |
| apogee height: | 2807 km |
| right ascension of ascending node: | 251.0150° |
| argument of perigee: | 260.6806° |
| revolutions per day: | 9.88353975 |
| mean anomaly at epoch: | 99.2078° |
| orbit number at epoch: | 11736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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