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 43677U 26075.76785674 +.00000000 +00000-0 +16343-3 0 00000
2 43677 98.0787 264.2520 0011682 72.1414 288.1083 15.02505109 04
| Epoch (UTC): | 16 March 2026 18:25:42 |
| Eccentricity: | 0.0011682 |
| inclination: | 98.0787° |
| perigee height: | 551 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 264.2520° |
| argument of perigee: | 72.1414° |
| revolutions per day: | 15.02505109 |
| mean anomaly at epoch: | 288.1083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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