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 46328U 26146.30477899 +.00000000 +00000-0 +11607-2 0 00009
2 46328 53.0261 281.9316 0012741 296.2140 63.7585 16.13489428 01
| Epoch (UTC): | 26 May 2026 07:18:52 |
| Eccentricity: | 0.0012741 |
| inclination: | 53.0261° |
| perigee height: | 229 km |
| apogee height: | 246 km |
| right ascension of ascending node: | 281.9316° |
| argument of perigee: | 296.2140° |
| revolutions per day: | 16.13489428 |
| mean anomaly at epoch: | 63.7585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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