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 65246U 26145.38615080 +.00000000 +00000-0 +22320-3 0 00007
2 65246 97.4475 188.1090 0002056 100.0240 260.1219 15.05656357 02
| Epoch (UTC): | 25 May 2026 09:16:03 |
| Eccentricity: | 0.0002056 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.1090° |
| argument of perigee: | 100.0240° |
| revolutions per day: | 15.05656357 |
| mean anomaly at epoch: | 260.1219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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