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 is defined by the following mean orbital elements,
1 27607U 26026.52965573 +.00000000 +00000-0 +30657-3 0 00007
2 27607 64.5515 207.1412 0073946 288.2690 71.0379 14.82601191 01
| Epoch (UTC): | 26 January 2026 12:42:42 |
| Eccentricity: | 0.0073946 |
| inclination: | 64.5515° |
| perigee height: | 569 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 207.1412° |
| argument of perigee: | 288.2690° |
| revolutions per day: | 14.82601191 |
| mean anomaly at epoch: | 71.0379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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