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 65457U 26145.30664134 +.00000000 +00000-0 +22810-3 0 00001
2 65457 97.4522 359.4877 0002189 76.5720 283.5751 15.05655546 01
| Epoch (UTC): | 25 May 2026 07:21:33 |
| Eccentricity: | 0.0002189 |
| inclination: | 97.4522° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.4877° |
| argument of perigee: | 76.5720° |
| revolutions per day: | 15.05655546 |
| mean anomaly at epoch: | 283.5751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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