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 45432U 26145.60982731 +.00000000 +00000-0 +20276-3 0 00005
2 45432 87.9160 10.3429 0001558 93.3230 266.8079 13.16052597 06
| Epoch (UTC): | 25 May 2026 14:38:09 |
| Eccentricity: | 0.0001558 |
| inclination: | 87.9160° |
| perigee height: | 1199 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 10.3429° |
| argument of perigee: | 93.3230° |
| revolutions per day: | 13.16052597 |
| mean anomaly at epoch: | 266.8079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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