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 26145.62528023 +.00000000 +00000-0 +96418-4 0 00001
2 58016 97.8882 216.9450 0001539 91.5259 268.6131 14.81696465 07
| Epoch (UTC): | 25 May 2026 15:00:24 |
| Eccentricity: | 0.0001539 |
| inclination: | 97.8882° |
| perigee height: | 623 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 216.9450° |
| argument of perigee: | 91.5259° |
| revolutions per day: | 14.81696465 |
| mean anomaly at epoch: | 268.6131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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