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 43440U 26150.84213073 +.00000000 +00000-0 +38194-3 0 00008
2 43440 97.0391 169.1031 0002588 356.1152 4.0066 15.24767564 06
| Epoch (UTC): | 30 May 2026 20:12:40 |
| Eccentricity: | 0.0002588 |
| inclination: | 97.0391° |
| perigee height: | 490 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 169.1031° |
| argument of perigee: | 356.1152° |
| revolutions per day: | 15.24767564 |
| mean anomaly at epoch: | 4.0066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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