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 43876U 26145.65671536 +.00000000 +00000-0 +10075-3 0 00004
2 43876 97.3597 51.6223 0001928 80.4993 279.6461 15.22856932 00
| Epoch (UTC): | 25 May 2026 15:45:40 |
| Eccentricity: | 0.0001928 |
| inclination: | 97.3597° |
| perigee height: | 496 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 51.6223° |
| argument of perigee: | 80.4993° |
| revolutions per day: | 15.22856932 |
| mean anomaly at epoch: | 279.6461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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