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 43877U 26145.61192884 +.00000000 +00000-0 +40463-3 0 00009
2 43877 97.3717 62.4488 0002533 78.2632 281.8899 15.40948013 08
| Epoch (UTC): | 25 May 2026 14:41:10 |
| Eccentricity: | 0.0002533 |
| inclination: | 97.3717° |
| perigee height: | 442 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 62.4488° |
| argument of perigee: | 78.2632° |
| revolutions per day: | 15.40948013 |
| mean anomaly at epoch: | 281.8899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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