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 65288U 26145.59026448 +.00000000 +00000-0 +38298-3 0 00001
2 65288 97.4463 198.1090 0002623 129.9937 230.1521 15.05655116 04
| Epoch (UTC): | 25 May 2026 14:09:58 |
| Eccentricity: | 0.0002623 |
| inclination: | 97.4463° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 198.1090° |
| argument of perigee: | 129.9937° |
| revolutions per day: | 15.05655116 |
| mean anomaly at epoch: | 230.1521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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