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 26037.67229943 +.00000000 +00000-0 +53503-3 0 00006
2 16719 82.5330 106.3246 0005185 58.0462 302.1296 15.56312160 06
| Epoch (UTC): | 06 February 2026 16:08:06 |
| Eccentricity: | 0.0005185 |
| inclination: | 82.5330° |
| perigee height: | 395 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 106.3246° |
| argument of perigee: | 58.0462° |
| revolutions per day: | 15.56312160 |
| mean anomaly at epoch: | 302.1296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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