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 64784U 26145.58286176 +.00000000 +00000-0 +00000-0 0 00003
2 64784 0.0487 85.3456 0003134 298.4148 65.2347 1.00272328 00
| Epoch (UTC): | 25 May 2026 13:59:19 |
| Eccentricity: | 0.0003134 |
| inclination: | 0.0487° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 85.3456° |
| argument of perigee: | 298.4148° |
| revolutions per day: | 1.00272328 |
| mean anomaly at epoch: | 65.2347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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