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 65438U 26145.32048734 +.00000000 +00000-0 +24416-3 0 00008
2 65438 97.4510 359.4675 0002714 84.7775 275.3762 15.05668766 07
| Epoch (UTC): | 25 May 2026 07:41:30 |
| Eccentricity: | 0.0002714 |
| inclination: | 97.4510° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.4675° |
| argument of perigee: | 84.7775° |
| revolutions per day: | 15.05668766 |
| mean anomaly at epoch: | 275.3762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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