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 15890U 26159.15566725 +.00000000 +00000-0 +43165-4 0 00009
2 15890 82.5259 69.9505 0019392 198.3869 161.6649 14.85853866 05
| Epoch (UTC): | 08 June 2026 03:44:09 |
| Eccentricity: | 0.0019392 |
| inclination: | 82.5259° |
| perigee height: | 597 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 69.9505° |
| argument of perigee: | 198.3869° |
| revolutions per day: | 14.85853866 |
| mean anomaly at epoch: | 161.6649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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