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 27619U 26118.99072625 +.00000000 +00000-0 +00000-0 0 00006
2 27619 65.4722 317.4564 0011649 248.6600 290.9476 2.13103611 05
| Epoch (UTC): | 28 April 2026 23:46:38 |
| Eccentricity: | 0.0011649 |
| inclination: | 65.4722° |
| perigee height: | 19100 km |
| apogee height: | 19159 km |
| right ascension of ascending node: | 317.4564° |
| argument of perigee: | 248.6600° |
| revolutions per day: | 2.13103611 |
| mean anomaly at epoch: | 290.9476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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