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 64000U 26145.43632704 +.00000000 +00000-0 +74027-3 0 00003
2 64000 42.9971 284.4541 0000260 26.5315 333.5550 15.27604632 02
| Epoch (UTC): | 25 May 2026 10:28:18 |
| Eccentricity: | 0.0000260 |
| inclination: | 42.9971° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 284.4541° |
| argument of perigee: | 26.5315° |
| revolutions per day: | 15.27604632 |
| mean anomaly at epoch: | 333.5550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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