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 65612U 26145.63715847 +.00000000 +00000-0 +15199-3 0 00000
2 65612 97.4457 214.1934 0002730 130.3297 229.8169 15.05658354 08
| Epoch (UTC): | 25 May 2026 15:17:30 |
| Eccentricity: | 0.0002730 |
| inclination: | 97.4457° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.1934° |
| argument of perigee: | 130.3297° |
| revolutions per day: | 15.05658354 |
| mean anomaly at epoch: | 229.8169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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