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 52659U 26145.46345903 +.00000000 +00000-0 -34204-4 0 00000
2 52659 53.2117 169.4168 0000757 62.4540 297.6529 15.08844820 03
| Epoch (UTC): | 25 May 2026 11:07:22 |
| Eccentricity: | 0.0000757 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 169.4168° |
| argument of perigee: | 62.4540° |
| revolutions per day: | 15.08844820 |
| mean anomaly at epoch: | 297.6529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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