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 43030U 26145.19427063 +.00000000 +00000-0 +18758-3 0 00005
2 43030 34.9957 50.3215 0002828 228.6989 131.3476 15.02528354 09
| Epoch (UTC): | 25 May 2026 04:39:44 |
| Eccentricity: | 0.0002828 |
| inclination: | 34.9957° |
| perigee height: | 557 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 50.3215° |
| argument of perigee: | 228.6989° |
| revolutions per day: | 15.02528354 |
| mean anomaly at epoch: | 131.3476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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