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 32258U 26145.50404500 +.00000000 +00000-0 +00000-0 0 00009
2 32258 0.0600 94.9373 0000394 289.4675 357.6406 1.00272198 01
| Epoch (UTC): | 25 May 2026 12:05:49 |
| Eccentricity: | 0.0000394 |
| inclination: | 0.0600° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 94.9373° |
| argument of perigee: | 289.4675° |
| revolutions per day: | 1.00272198 |
| mean anomaly at epoch: | 357.6406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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