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 64955U 26145.09537340 +.00000000 +00000-0 +23488-3 0 00009
2 64955 97.4540 9.0375 0002240 85.0286 275.1197 15.05657206 00
| Epoch (UTC): | 25 May 2026 02:17:20 |
| Eccentricity: | 0.0002240 |
| inclination: | 97.4540° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.0375° |
| argument of perigee: | 85.0286° |
| revolutions per day: | 15.05657206 |
| mean anomaly at epoch: | 275.1197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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