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 55332U 26145.21802425 +.00000000 +00000-0 +11896-3 0 00001
2 55332 42.9971 216.8176 0000255 311.2445 48.8385 15.27600926 09
| Epoch (UTC): | 25 May 2026 05:13:57 |
| Eccentricity: | 0.0000255 |
| inclination: | 42.9971° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 216.8176° |
| argument of perigee: | 311.2445° |
| revolutions per day: | 15.27600926 |
| mean anomaly at epoch: | 48.8385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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