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 64933U 26145.57719052 +.00000000 +00000-0 +20733-3 0 00000
2 64933 97.4476 9.4545 0001719 70.6504 289.4909 15.05656467 07
| Epoch (UTC): | 25 May 2026 13:51:09 |
| Eccentricity: | 0.0001719 |
| inclination: | 97.4476° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.4545° |
| argument of perigee: | 70.6504° |
| revolutions per day: | 15.05656467 |
| mean anomaly at epoch: | 289.4909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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