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 27607U 02058C 25341.07111585 .00003254 00000-0 40586-3 0 9990
2 27607 64.5544 3.1188 0071943 297.6413 61.7401 14.82353094235973
| Epoch (UTC): | 07 December 2025 01:42:24 |
| Eccentricity: | 0.0071943 |
| inclination: | 64.5544° |
| perigee height: | 571 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 3.1188° |
| argument of perigee: | 297.6413° |
| revolutions per day: | 14.82353094 |
| mean anomaly at epoch: | 61.7401° |
| orbit number at epoch: | 23597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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