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 27386U 02009A 23033.17569642 .00000224 00000-0 87274-4 0 9998
2 27386 98.2132 8.8615 0001217 89.0489 281.4975 14.38233193 96558
| Epoch (UTC): | 02 February 2023 04:13:00 |
| Eccentricity: | 0.0001217 |
| inclination: | 98.2132° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 8.8615° |
| argument of perigee: | 89.0489° |
| revolutions per day: | 14.38233193 |
| mean anomaly at epoch: | 281.4975° |
| orbit number at epoch: | 9655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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