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 64554U 26145.28598051 +.00000000 +00000-0 +66780-3 0 00003
2 64554 97.4614 262.3092 0001733 63.2491 296.8926 15.29826623 06
| Epoch (UTC): | 25 May 2026 06:51:48 |
| Eccentricity: | 0.0001733 |
| inclination: | 97.4614° |
| perigee height: | 475 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 262.3092° |
| argument of perigee: | 63.2491° |
| revolutions per day: | 15.29826623 |
| mean anomaly at epoch: | 296.8926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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