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 43770U 26145.59282205 +.00000000 +00000-0 +42389-3 0 00004
2 43770 97.4402 205.9301 0010165 73.6783 286.5572 15.26140361 00
| Epoch (UTC): | 25 May 2026 14:13:39 |
| Eccentricity: | 0.0010165 |
| inclination: | 97.4402° |
| perigee height: | 480 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 205.9301° |
| argument of perigee: | 73.6783° |
| revolutions per day: | 15.26140361 |
| mean anomaly at epoch: | 286.5572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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