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 65397U 26145.60412611 +.00000000 +00000-0 +14616-3 0 00003
2 65397 97.4488 16.9661 0002533 78.0152 282.1359 15.05654448 09
| Epoch (UTC): | 25 May 2026 14:29:56 |
| Eccentricity: | 0.0002533 |
| inclination: | 97.4488° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9661° |
| argument of perigee: | 78.0152° |
| revolutions per day: | 15.05654448 |
| mean anomaly at epoch: | 282.1359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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