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 32487U 26145.29844975 +.00000000 +00000-0 +00000-0 0 00003
2 32487 0.0277 259.0408 0002589 173.1080 277.4343 1.00273465 02
| Epoch (UTC): | 25 May 2026 07:09:46 |
| Eccentricity: | 0.0002589 |
| inclination: | 0.0277° |
| perigee height: | 35775 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 259.0408° |
| argument of perigee: | 173.1080° |
| revolutions per day: | 1.00273465 |
| mean anomaly at epoch: | 277.4343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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