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 23037.00781223 .00000267 00000-0 10144-3 0 9993
2 27386 98.2142 12.5269 0001231 89.8859 310.4619 14.38235805 97103
| Epoch (UTC): | 06 February 2023 00:11:14 |
| Eccentricity: | 0.0001231 |
| inclination: | 98.2142° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 12.5269° |
| argument of perigee: | 89.8859° |
| revolutions per day: | 14.38235805 |
| mean anomaly at epoch: | 310.4619° |
| orbit number at epoch: | 9710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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