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 56334U 26145.45931421 +.00000000 +00000-0 +29530-3 0 00003
2 56334 97.4457 146.5956 0002006 97.4838 262.6617 15.05658875 02
| Epoch (UTC): | 25 May 2026 11:01:24 |
| Eccentricity: | 0.0002006 |
| inclination: | 97.4457° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.5956° |
| argument of perigee: | 97.4838° |
| revolutions per day: | 15.05658875 |
| mean anomaly at epoch: | 262.6617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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