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 26039.60112058 +.00000000 +00000-0 +42646-3 0 00005
2 16719 82.5329 104.3076 0005056 52.2101 307.9610 15.56441829 04
| Epoch (UTC): | 08 February 2026 14:25:36 |
| Eccentricity: | 0.0005056 |
| inclination: | 82.5329° |
| perigee height: | 395 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 104.3076° |
| argument of perigee: | 52.2101° |
| revolutions per day: | 15.56441829 |
| mean anomaly at epoch: | 307.9610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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