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 26065.35426226 +.00000000 +00000-0 +68273-4 0 00008
2 16720 82.5560 150.1525 0019929 31.4764 35.8359 14.85664980 02
| Epoch (UTC): | 06 March 2026 08:30:08 |
| Eccentricity: | 0.0019929 |
| inclination: | 82.5560° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 150.1525° |
| argument of perigee: | 31.4764° |
| revolutions per day: | 14.85664980 |
| mean anomaly at epoch: | 35.8359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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