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 16719U 26039.21536931 +.00000000 +00000-0 +49091-3 0 00003
2 16719 82.5329 104.7110 0005097 53.7128 306.4597 15.56420485 00
| Epoch (UTC): | 08 February 2026 05:10:07 |
| Eccentricity: | 0.0005097 |
| inclination: | 82.5329° |
| perigee height: | 395 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 104.7110° |
| argument of perigee: | 53.7128° |
| revolutions per day: | 15.56420485 |
| mean anomaly at epoch: | 306.4597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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