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 23089.67541462 .00000604 00000-0 21206-3 0 9998
2 27386 98.2232 62.9381 0001390 85.6448 336.7141 14.38301019104674
| Epoch (UTC): | 30 March 2023 16:12:35 |
| Eccentricity: | 0.0001390 |
| inclination: | 98.2232° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 62.9381° |
| argument of perigee: | 85.6448° |
| revolutions per day: | 14.38301019 |
| mean anomaly at epoch: | 336.7141° |
| orbit number at epoch: | 10467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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