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 51787U 26144.91376315 +.00000000 +00000-0 +69686-4 0 00002
2 51787 53.2131 6.9360 0001462 56.6074 303.5058 15.08844499 06
| Epoch (UTC): | 24 May 2026 21:55:49 |
| Eccentricity: | 0.0001462 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 6.9360° |
| argument of perigee: | 56.6074° |
| revolutions per day: | 15.08844499 |
| mean anomaly at epoch: | 303.5058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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