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 65242U 26145.13140554 +.00000000 +00000-0 +33365-4 0 00007
2 65242 97.4492 187.9940 0001731 134.3577 225.7792 15.05646179 04
| Epoch (UTC): | 25 May 2026 03:09:13 |
| Eccentricity: | 0.0001731 |
| inclination: | 97.4492° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 187.9940° |
| argument of perigee: | 134.3577° |
| revolutions per day: | 15.05646179 |
| mean anomaly at epoch: | 225.7792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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