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 16720U 26088.18552412 +.00000000 +00000-0 +54412-4 0 00001
2 16720 82.5517 128.7888 0018044 315.1348 108.0196 14.85684970 07
| Epoch (UTC): | 29 March 2026 04:27:09 |
| Eccentricity: | 0.0018044 |
| inclination: | 82.5517° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 128.7888° |
| argument of perigee: | 315.1348° |
| revolutions per day: | 14.85684970 |
| mean anomaly at epoch: | 108.0196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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