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 27665U 03005C 25198.42582799 .00000025 00000-0 42952-4 0 9998
2 27665 39.5735 192.2971 0008007 22.8677 133.7596 14.29406643173114
| Epoch (UTC): | 17 July 2025 10:13:11 |
| Eccentricity: | 0.0008007 |
| inclination: | 39.5735° |
| perigee height: | 788 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 192.2971° |
| argument of perigee: | 22.8677° |
| revolutions per day: | 14.29406643 |
| mean anomaly at epoch: | 133.7596° |
| orbit number at epoch: | 17311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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