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 65914U 26145.43948059 +.00000000 +00000-0 +84090-3 0 00002
2 65914 53.1573 168.8435 0001226 88.2666 271.8475 15.30198952 00
| Epoch (UTC): | 25 May 2026 10:32:51 |
| Eccentricity: | 0.0001226 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.8435° |
| argument of perigee: | 88.2666° |
| revolutions per day: | 15.30198952 |
| mean anomaly at epoch: | 271.8475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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