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 43798U 26145.45368532 +.00000000 +00000-0 +65173-3 0 00003
2 43798 97.4383 223.2697 0003303 299.1535 60.9384 15.47834234 02
| Epoch (UTC): | 25 May 2026 10:53:18 |
| Eccentricity: | 0.0003303 |
| inclination: | 97.4383° |
| perigee height: | 421 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 223.2697° |
| argument of perigee: | 299.1535° |
| revolutions per day: | 15.47834234 |
| mean anomaly at epoch: | 60.9384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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