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 27609U 02058E 25196.56129509 .00000168 00000-0 40356-4 0 9996
2 27609 64.5562 294.9861 0050519 292.3660 67.2096 14.80877184217830
| Epoch (UTC): | 15 July 2025 13:28:15 |
| Eccentricity: | 0.0050519 |
| inclination: | 64.5562° |
| perigee height: | 591 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 294.9861° |
| argument of perigee: | 292.3660° |
| revolutions per day: | 14.80877184 |
| mean anomaly at epoch: | 67.2096° |
| orbit number at epoch: | 21783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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