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 53787U 26145.43033538 +.00000000 +00000-0 +43506-4 0 00002
2 53787 53.2131 289.4553 0001250 107.6433 252.4695 15.08835176 02
| Epoch (UTC): | 25 May 2026 10:19:40 |
| Eccentricity: | 0.0001250 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.4553° |
| argument of perigee: | 107.6433° |
| revolutions per day: | 15.08835176 |
| mean anomaly at epoch: | 252.4695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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