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 65446U 26145.40910288 +.00000000 +00000-0 +45360-3 0 00009
2 65446 97.4487 359.6569 0001957 76.7187 283.4258 15.05658625 02
| Epoch (UTC): | 25 May 2026 09:49:06 |
| Eccentricity: | 0.0001957 |
| inclination: | 97.4487° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.6569° |
| argument of perigee: | 76.7187° |
| revolutions per day: | 15.05658625 |
| mean anomaly at epoch: | 283.4258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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