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 58016U 26100.17567257 +.00000000 +00000-0 +11583-3 0 00003
2 58016 97.8910 172.1693 0001441 98.7563 261.3813 14.81633312 09
| Epoch (UTC): | 10 April 2026 04:12:58 |
| Eccentricity: | 0.0001441 |
| inclination: | 97.8910° |
| perigee height: | 623 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 172.1693° |
| argument of perigee: | 98.7563° |
| revolutions per day: | 14.81633312 |
| mean anomaly at epoch: | 261.3813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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