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 26087.69692941 +.00000000 +00000-0 +34072-3 0 00004
2 43187 97.5425 352.9968 0007453 298.9946 61.0539 15.15836786 09
| Epoch (UTC): | 28 March 2026 16:43:34 |
| Eccentricity: | 0.0007453 |
| inclination: | 97.5425° |
| perigee height: | 513 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 352.9968° |
| argument of perigee: | 298.9946° |
| revolutions per day: | 15.15836786 |
| mean anomaly at epoch: | 61.0539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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