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 64864U 26145.41045662 +.00000000 +00000-0 +41544-3 0 00008
2 64864 97.4488 0.7760 0001943 87.4745 272.6705 15.05657627 05
| Epoch (UTC): | 25 May 2026 09:51:03 |
| Eccentricity: | 0.0001943 |
| inclination: | 97.4488° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.7760° |
| argument of perigee: | 87.4745° |
| revolutions per day: | 15.05657627 |
| mean anomaly at epoch: | 272.6705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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