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 64102U 26145.40656983 +.00000000 +00000-0 +97444-3 0 00006
2 64102 53.1618 30.0363 0001322 90.1647 269.9507 15.34419506 05
| Epoch (UTC): | 25 May 2026 09:45:27 |
| Eccentricity: | 0.0001322 |
| inclination: | 53.1618° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 30.0363° |
| argument of perigee: | 90.1647° |
| revolutions per day: | 15.34419506 |
| mean anomaly at epoch: | 269.9507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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