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 65057U 26145.62389707 +.00000000 +00000-0 +41203-3 0 00009
2 65057 97.4471 222.6354 0002770 153.5774 206.5595 15.05660024 00
| Epoch (UTC): | 25 May 2026 14:58:24 |
| Eccentricity: | 0.0002770 |
| inclination: | 97.4471° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.6354° |
| argument of perigee: | 153.5774° |
| revolutions per day: | 15.05660024 |
| mean anomaly at epoch: | 206.5595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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