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 26076.19681030 +.00000000 +00000-0 +42420-4 0 00004
2 16720 82.5540 140.0084 0018996 356.2988 65.5513 14.85675236 05
| Epoch (UTC): | 17 March 2026 04:43:24 |
| Eccentricity: | 0.0018996 |
| inclination: | 82.5540° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 140.0084° |
| argument of perigee: | 356.2988° |
| revolutions per day: | 14.85675236 |
| mean anomaly at epoch: | 65.5513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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