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 43187U 26106.97067015 +.00000000 +00000-0 +15806-3 0 00009
2 43187 97.5415 12.1423 0007724 216.8968 143.1735 15.16066098 05
| Epoch (UTC): | 16 April 2026 23:17:45 |
| Eccentricity: | 0.0007724 |
| inclination: | 97.5415° |
| perigee height: | 512 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 12.1423° |
| argument of perigee: | 216.8968° |
| revolutions per day: | 15.16066098 |
| mean anomaly at epoch: | 143.1735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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