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 53446U 26145.59616955 +.00000000 +00000-0 +64130-3 0 00006
2 53446 97.5598 274.3026 0003056 125.8740 234.2803 15.64000615 02
| Epoch (UTC): | 25 May 2026 14:18:29 |
| Eccentricity: | 0.0003056 |
| inclination: | 97.5598° |
| perigee height: | 374 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 274.3026° |
| argument of perigee: | 125.8740° |
| revolutions per day: | 15.64000615 |
| mean anomaly at epoch: | 234.2803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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