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 26068.31783198 +.00000000 +00000-0 +60695-4 0 00001
2 16720 82.5555 147.3801 0019707 22.1171 45.7402 14.85668263 01
| Epoch (UTC): | 09 March 2026 07:37:40 |
| Eccentricity: | 0.0019707 |
| inclination: | 82.5555° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 147.3801° |
| argument of perigee: | 22.1171° |
| revolutions per day: | 14.85668263 |
| mean anomaly at epoch: | 45.7402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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